Copenhagen Suborbitals: Difference between revisions
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{{short description|Amateur crowdfunded |
{{short description|Amateur crowdfunded human space programme}} |
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{{Advert|date=October 2017}} |
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{{Infobox company |
{{Infobox company |
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| name |
| name = Copenhagen Suborbitals |
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| logo |
| logo = Copenhagen Suborbitals logo.svg |
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| type |
| type = [[Non-profit]], open source, amateur, all-volunteer organisation |
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| industry |
| industry = [[Aerospace engineering|Aerospace]] |
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| caption |
| caption = |
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| foundation |
| foundation = {{Start date and age|2008|05|01|df=yes}} |
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| founders |
| founders = [[Kristian von Bengtson]]<br>[[Peter Madsen (inventor)|Peter Madsen]] |
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| location |
| location = [[Refshaleøen, Copenhagen]], [[Denmark]] {{coord|55|41|29.1|N|12|37|1.21|E|region:DK|display=title}} |
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| key_people = Chairman: Jørgen Skyt<br>Vice Chairman: Storm Boysen<br>Executive Officer: Niels Johansen<br>Communication Director: Mads Wilson<br>Space Strategist: Thomas Pedersen<br>Space medicine: Niels Foldager |
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| key_people = Chairman: Carsten Olsen |
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| num_employees = 55<ref>{{cite web|url=http://ing.dk/artikel/dansk-rumrakets-motor-imploderede-135281|title=Dansk rumrakets motor imploderede - Ingeniøren|date=2 January 2013|website=Ing.dk|access-date=11 August 2017}}</ref> (all [[volunteering]])<ref name="CS_FAQ">{{cite web|title=FAQ copenhagensuborbitals.com|url=https://copenhagensuborbitals.com/faq.php|publisher=copenhagensuborbitals.com|access-date=2017-05-23|archive-url=https://web.archive.org/web/20121129045524/http://www.copenhagensuborbitals.com/faq.php|archive-date=2012-11-29|url-status=dead}}</ref> |
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| products = |
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Executive Officer: Niels Johansen |
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| homepage = {{URL|https://copenhagensuborbitals.com/}} |
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Communication Director: Mads Wilson |
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Space Strategist: Thomas Pedersen |
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Space medicine: Niels Foldager |
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| num_employees = 55<ref>{{cite web|url=http://ing.dk/artikel/dansk-rumrakets-motor-imploderede-135281|title=Dansk rumrakets motor imploderede - Ingeniøren|date=2 January 2013|website=Ing.dk|accessdate=11 August 2017}}</ref> (all [[volunteering]])<ref name=CS_FAQ>{{cite web|title=FAQ copenhagensuborbitals.com|url=https://copenhagensuborbitals.com/faq.php|publisher=copenhagensuborbitals.com}}</ref> |
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| products = |
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| homepage = {{url|https://copenhagensuborbitals.com/}} |
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}} |
}} |
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{{Private spaceflight}} |
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'''Copenhagen Suborbitals''' is an amateur crowd-funded manned space programme. Since its beginning in 2008, Copenhagen Suborbitals has flown five home-built rockets and two mock-up space capsules. Their stated goal is to have one of the members fly into space (above 100 km), on a [[sub-orbital spaceflight]], in a space capsule on the Spica rocket. The organisation was founded by [[Kristian von Bengtson]] and by [[Peter Madsen]], who was convicted of the [[murder of Kim Wall]] in 2017. Peter Madsen was excluded from Copenhagen Suborbitals in 2014.<ref>https://copenhagensuborbitals.com/statement-former-copenhagen-suborbitals-member-peter-madsen/</ref> The organization successfully launched its Nexø II rocket in summer 2018.<ref>https://ing.dk/artikel/succes-nexoe-ii-landet-med-faldskaerm-efter-tur-paa-6500-meter-213612</ref><ref>https://www.dr.dk/nyheder/viden/teknologi/i-morgen-sker-det-danskere-affyrer-300-kg-tung-raket-over-oestersoeen</ref> |
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'''Copenhagen Suborbitals''' is a [[Crowd funded|crowd-funded]] human space program. It has flown six home-built rockets and capsules since 2011.<ref>{{Cite web |title=About us – Copenhagen Suborbitals |url=https://copenhagensuborbitals.com/about-us/ |access-date=2024-02-09 |language=en-US}}</ref> The organization successfully launched its Nexø II rocket in the summer of 2018.<ref>{{Cite web |date=August 4, 2018 |title=Succes: Nexø II landet med faldskærm efter tur på 6.500 meter |url=https://ing.dk/artikel/succes-nexoe-ii-landet-med-faldskaerm-efter-tur-paa-6500-meter-213612 |website=Ingeniøren}}</ref><ref>{{Cite web |title=I morgen sker det: Danskere affyrer 300 kg tung raket over Østersøen |url=https://www.dr.dk/nyheder/viden/teknologi/i-morgen-sker-det-danskere-affyrer-300-kg-tung-raket-over-oestersoeen |website=DR|date=3 August 2018}}</ref> Its stated goal is to have one of its members reach space ([[Kármán line|above 100 km]]) on a [[sub-orbital spaceflight]]. The organization was founded by [[Kristian von Bengtson]] and [[Peter Madsen]].<ref>{{Cite web |last=Wilson |first=Mads |date=2017-09-06 |title=Our statement on former Copenhagen Suborbitals member Peter Madsen – Copenhagen Suborbitals |url=https://copenhagensuborbitals.com/statement-former-copenhagen-suborbitals-member-peter-madsen/ |url-status=dead |archive-url=https://web.archive.org/web/20170907030129/https://copenhagensuborbitals.com/statement-former-copenhagen-suborbitals-member-peter-madsen/ |archive-date=2017-09-07 |website=Copenhagen Suborbitals}}</ref> |
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As an amateur organisation, the 55 members use their spare time on the project, while at the same time having regular day-jobs. At the annual general assembly, they elect a chairman and boardmembers. Currently (2019), the chairman is Carsten Olsen.<ref>{{Cite news|url=https://copenhagensuborbitals.com/mission/the-team/|title=The Team - Copenhagen Suborbitals|work=Copenhagen Suborbitals|access-date=2017-05-09|language=en-US}}</ref> |
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As of September 2024, the program has 63 volunteers who elect a chairman and board members at their annual general assemblies. The chairman is Jørgen Skyt. |
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==Astronauts== |
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As of 2017, three members are candidates to become the first astronaut to fly on the Spica rocket: |
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* Mads Stenfatt |
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* Anna Olsen |
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* Carsten Olsen (father of Anna Olsen) |
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==Crowd-funding== |
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Funding comes from worldwide donations, many of them on a monthly basis as members of Copenhagen Suborbitals Support. This is augmented by fees from speeches and lectures done by group members. Also, in 2015 Copenhagen Suborbitals taught students from the National Technical University of Singapore in basic rocket design, for which the group received a fee. All income goes directly to the group's project, with all members working completely for free. |
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==Sea launch== |
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[[File:TPE IMG 3516.jpg|thumb|The floating launch platform ''MLP Sputnik'' with HEAT 1X Tycho Brahe, photographed June 2011]] |
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[[Image:Vostok011.jpg|thumb|right|M/S Vostok in 2012.]] |
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A unique aspect of the project is that all rockets are launched at sea. As a non-governmental, non-commercial organisation, flying rockets from land is virtually impossible anywhere in the world. Therefore, the group conducts all flights from a mobile launch platform, MLP Sputnik, in international waters on the [[Baltic Sea]], east of the [[Denmark|Danish]] island [[Bornholm]]. The port of [[Nexø]] becomes the Copenhagen Suborbitals fleet's homeport during the summer launch missions, affectionately dubbed Spaceport Nexø. The group operates three ships: |
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* MLP Sputnik: A twin-hull, self-propelled mobile, launch platform that has carried all the group's rockets and space capsules since 2010. Owned by Copenhagen Suborbitals. |
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* M/S Vostok. Originally built as a rescue vessel for the German Coast Guard, she's the command ship during launch and recovery, acting as flagship of the mission fleet. Owned by Copenhagen Suborbitals. |
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* M/S Antares. Support ship. Owned by Copenhagen Suborbitals member Carsten Olsen |
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During missions, the three vessels are augmented by multiple ships (often including the patrol vessel MHV903 Hjortø from the [[Home Guard (Denmark)|Danish Naval Home Guard]]), boats and aircraft. When not deployed, Vostok and Sputnik are based at Copenhagen Suborbitals HQ in the port of [[Copenhagen]]. |
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==History== |
==History== |
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[[File:CopenhagenSuborbitalCrew.jpg|thumb|right|The crew gathered in front of the static rocket test setup in November 2011]] |
[[File:CopenhagenSuborbitalCrew.jpg|thumb|right|The crew gathered in front of the static rocket test setup in November 2011]] |
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Copenhagen Suborbitals was founded in 2008 by [[Kristian von Bengtson]] and |
Copenhagen Suborbitals was founded in 2008 by [[Kristian von Bengtson]] and [[Peter Madsen (inventor)|Peter Madsen]] as a non-profit, crowd-funded project that discussed most of their operations on blogs<ref name="Wired_blog">{{cite web|title=ROCKET SHOP|url=https://www.wired.com/wiredscience/rocketshop|website=Wired.com|access-date=25 November 2011}}</ref><ref>{{cite web|title=Rumfart på den anden måde|url=http://ing.dk/blogs/rumfartpaadenandenmaade|publisher=ing.dk|access-date=25 November 2011|archive-date=31 October 2010|archive-url=https://web.archive.org/web/20101031123530/http://ing.dk/blogs/rumfartpaadenandenmaade|url-status=dead}}</ref> and lectures.<ref>{{cite web|title=TEDxCopenhagen - Kristian von Bengtson - Danes in space|url=https://www.youtube.com/watch?v=ua9oGxNNGd0 |archive-url=https://ghostarchive.org/varchive/youtube/20211215/ua9oGxNNGd0 |archive-date=2021-12-15 |url-status=live|publisher=TED X|access-date=27 November 2011}}{{cbignore}}</ref> |
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On 23 February 2014 the board of Copenhagen Suborbitals announced that Kristian von Bengtson had left the group, after falling out with Madsen. |
On 23 February 2014, the board of Copenhagen Suborbitals announced that Kristian von Bengtson had left the group, after falling out with Madsen. Madsen left in June 2014.<ref>{{Cite web|url=https://copenhagensuborbitals.com/statement-former-copenhagen-suborbitals-member-peter-madsen/|title=Our statement on former Copenhagen Suborbitals member Peter Madsen – Copenhagen Suborbitals|website=copenhagensuborbitals.com|language=en-GB|access-date=2018-10-08|archive-date=2018-06-11|archive-url=https://web.archive.org/web/20180611030936/https://copenhagensuborbitals.com/statement-former-copenhagen-suborbitals-member-peter-madsen/|url-status=dead}}</ref> |
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==Rockets and engines== |
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==Suborbital space flight profile== |
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===Spica=== |
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In 2014, Copenhagen Suborbitals designed a basic first crewed rocket and space capsule. They named it Spica, and it is planned to stand 12–14 m tall with a diameter of 950 mm.<ref>{{Cite web |title=Spica – Copenhagen Suborbitals |url=https://copenhagensuborbitals.com/missions/spica/ |access-date=2024-02-09 |language=en-US}}</ref> As of late September 2024, two pressure hardened 950mm steel tanks have been constructed and the development of the BPM-25 engine class is well underway. |
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Originally, the Spica rocket was planned to be powered by the BPM-100 class, but due to internal manufacturing troubles, the BPM-25 was eventually decided on as the engine to power the rocket.<ref name=":1">{{Cite web |last=Wilson |first=Mads |date=2023-07-31 |title=Rocket Engines: Is Bigger = Worse? – Copenhagen Suborbitals |url=https://copenhagensuborbitals.com/rocket-engines-is-bigger-worse/ |access-date=2024-02-09 |language=en-US}}</ref> Though it is weaker, it provides several advantages through greater roll authority and flow control. The BPM-25 engines, unlike the BPM-100, will have to be clustered in order to achieve the necessary thrust to launch Spica to the desired altitude. The BPM-25 provides 25 kN of thrust.<ref>{{Cite web |last=Wilson |first=Mads |date=2023-05-31 |title=Introducing the BPM-25 engine – Copenhagen Suborbitals |url=https://copenhagensuborbitals.com/introducing-the-bpm-25-engine/ |access-date=2024-02-09 |language=en-US}}</ref> Similar to the BPM-100 engine, it uses liquid oxygen as oxidizer and ethanol as fuel. Spica will maneuver by thrust vectoring on its BPM-25 engines. |
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[[File:Flightpath02.jpg|right|thumb|Drawing of the flight path]] |
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From the launch site on the Baltic Sea, the Spica rocket will carry the Spica capsule and the astronaut into space above 100 km. The capsule will separate and fall back to earth, where it will be decelerated by a [[ballute]] and [[parachute]]s, and land back in the Baltic Sea. |
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The rocket will be fully guided by home-built electronics and software. Many of the systems and technology planned for use on this rocket were previously tested and proven on the smaller Nexø class rockets in during the 2016 to 2018 period.<ref name=":0" /> The space capsule will be of a tubular design similar to its predecessor [[HEAT 1X Tycho Brahe|Tycho Brahe]]. While the Spica capsule has not entered more than marginal construction as of 2024, CS plans on first building a boilerplate capsule to test on the ground before moving onto the real article.<ref>{{Cite web |title=Spica Capsule – Copenhagen Suborbitals |url=https://copenhagensuborbitals.com/missions/spica-capsule/ |access-date=2024-02-09 |language=en-US}}</ref> |
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==Facilities== |
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===BPM-2 and BPM-5=== |
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[[File:Copenhagen Suborbitals Hangar 02-13-2010.jpg|thumb|Interior of the HAB building]] |
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During the 2016-2018 period, the group designed, built and tested a series of smaller engines with a nominal thrust of 2 and 5 kN - the BPM(Bi-Propellant Motor)-2 class and BPM-5 class respectively. Nexø I launched under the power of a BPM-5 on July 23rd, 2016.<ref>{{Cite web |title=Nexø I – Copenhagen Suborbitals |url=https://copenhagensuborbitals.com/missions/nexo-i/ |access-date=2024-02-09 |language=en-US}}</ref> On August 4, 2018, just as the Nexø I, Nexø II was launched under the power of a BPM-5.<ref name=":0">{{Cite web |title=Nexø II – Copenhagen Suborbitals |url=https://copenhagensuborbitals.com/missions/nexo-ii/ |access-date=2024-02-09 |language=en-US}}</ref> The Nexø class was primarily intended to serve as a technology demonstrator ahead of the development of Spica.<ref name=":0" /> The BPM engines are bi-liquid rocket engines using [[LOX]] and [[ethanol]], [[Regenerative cooling (rocket)|regeneratively cooled]] by the ethanol fuel.<ref>{{Cite web |title=Spica Engine – Copenhagen Suborbitals |url=https://copenhagensuborbitals.com/missions/spica-engine/ |access-date=2024-02-09 |language=en-US}}</ref> |
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CS started on a barge called M/S Half Machine in [[Port of Copenhagen]]. On 1 August 2009 they relocated to its base and office on [[Refshaleøen]], the old [[Burmeister & Wain]] shipyard, in [[Copenhagen]]. Their workshop is dubbed HAB 2 ("Horizontal Assembly Building" as a reference to NASA's VAB). |
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The BPM-2 was primarily intended to serve as a test article for the CS test stand and manufacturing methods, and was never intended to launch a rocket. The BPM-2 engine was static fired 4 separate times on May 2nd, 2015.<ref name=":3">{{Cite web |title=Copenhagen Suborbitals BPM-2 Test |url=https://www.mach5lowdown.com/2015/04/13/copenhagen-suborbitals-bpm-2-test/ |access-date=2024-02-10 |language=en-US}}</ref> |
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==Rockets and engines== |
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The tests were successful, with results exceeding expectations. Different fuel additives (such as [[TEOS]]) as well as different jet vane materials were also tested. The 2015 test firings used passive pressure blow-down.<ref name=":3" /> |
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===Spica=== |
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In 2014, Copenhagen Suborbitals settled on the basic design for their first crewed rocket and space capsule. The rocket will be named Spica, and will stand 12–14 m tall with a diameter of 950 mm. It will be powered by the BPM-100 engine class, using liquid oxygen as oxidizer and ethanol as fuel, producing 100 kilonewtons of thrust. It's likely to feature pressure-blow-down tanks, optimised by a dynamic pressure regulation (DPR) system, but turbo pumps are also a possibility, albeit they are difficult to build. Flight control will be thrust vectoring via a gimbal engine. The rocket will be fully guided by home-built electronics and software. Most of the systems and technology will initially be tested on the smaller Nexø class rockets in 2016/18. The space capsule will be of a tubular design as its predecessor Tycho Brahe, but its greater diameter will allow the astronaut to assume a sitting position during launch and re-entry, in order to withstand the G-forces. |
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===BPM-2 and BPM-5=== |
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In 2014/2015 the group designed, built and tested a series of smaller engines with a nominal thrust of 2 and 5 kN. |
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The BPM-5 class will fly on the Nexø I and II rockets in 2016/2018, paving the way for the much bigger Spica rocket and engine. The purpose was to validate the performance and operation of the group's new engine design direction. The tests were highly successful, with results exceeding expectations. Different fuel additives (such as [[TEOS]]) as well as different jet vane material were also tested. |
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The BPM engines are bi-liquid rocket engines using [[LOX]] and [[ethanol]], [[Regenerative cooling (rocket)|regeneratively cooled]] by the ethanol fuel. The spring/summer 2015 test firings used passive pressure blow-down, and in winter 2015/2016 will see the test firings continue with a dynamic pressure (DPR) regulation system, which then will fly on the Nexø II rocket in spring 2018. |
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No more development or use for BPM-2 or -5 engines is planned. CS has primarily moved on to the use of the BPM-25 ahead of the planned development of the Spica rocket.<ref name=":1" /> |
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===Engines and propellant 2008 - 2014=== |
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===Engines and propellant 2008–2014=== |
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From 2008 to 2012, the group based the work on a [[hybrid rocket]], using [[liquid oxygen]] (LOX) as [[oxidizer]]. Originally, the HEAT-1X rocket was to be fuelled by [[paraffin wax]], but a ground test 28 February 2010 revealed that some of the paraffin wax had only partially melted, instead of evaporating. The result was that HEAT-1X had less power than expected. A ground test firing of HEAT-1X-P (P for [[polyurethane]]) was conducted 16 May 2010. It was positive, the polyurethane had the right power but showed heavy [[oscillation]]. Until 2011 the group had performed more than 30 tests of various engine types at their [[rocket engine test facility]] at [[Refshaleøen, Copenhagen|Refshaleøen]]. In fall of 2012 a concept engine using [[white fuming nitric acid]] and [[furfuryl alcohol]] was tried using a static test setup.<ref>{{cite web | url=http://ing.dk/artikel/132056-spectra-testen | title=Spectra-testen | accessdate=September 10, 2012 | author=Madsen, Peter}}</ref> In 2012 it was decided to switch to bi-propellant, liquid-fuelled engines running on liquid oxygen and ethanol. |
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From 2008 to 2012, the group based the work on a [[hybrid rocket]], using [[liquid oxygen]] (LOX) as [[oxidizer]].<ref name=":4">{{Cite web |title=HEAT-1X – Copenhagen Suborbitals |url=https://copenhagensuborbitals.com/missions/heat-1x/ |access-date=2024-01-09 |language=en-US}}</ref> Originally, the HEAT-1X rocket was to be fueled by [[paraffin wax]], but a ground test 28 February 2010 revealed that some of the paraffin wax had only partially melted, instead of evaporating. The result was that HEAT-1X had less power than expected. A ground test firing of HEAT-1X-P (P for [[polyurethane]]) was conducted 16 May 2010. The polyurethane had the impulse required, but showed heavy [[oscillation]].<ref>{{Citation |title=Copenhagen Suborbitals HEAT-1XP |url=https://www.youtube.com/watch?v=EGLvCXbWcMk |access-date=2024-02-10 |language=en}}</ref> Until 2011 the group had performed more than 30 tests of various engine types at their [[rocket engine test facility]] at [[Refshaleøen, Copenhagen|Refshaleøen]].<ref>{{Cite web |date=2013-08-15 |title=DIY rockets {{!}} CNN Business |url=https://www.cnn.com/2013/08/15/tech/gallery/diy-rockets/index.html |access-date=2024-02-10 |website=CNN |language=en}}</ref> In fall of 2012 a concept engine using [[white fuming nitric acid]] and [[furfuryl alcohol]] was tried using a static test setup.<ref>{{cite web |url=http://ing.dk/artikel/132056-spectra-testen |title=Spectra-testen |access-date=September 10, 2012 |author=Madsen, Peter |archive-url=https://web.archive.org/web/20120912034944/http://ing.dk/artikel/132056-spectra-testen |archive-date=September 12, 2012 |url-status=dead}}</ref> In 2012 a decision was made to switch to bi-propellant, liquid-fueled engines running on liquid oxygen and ethanol. This evolved into the BPM(Bi-Propellant Motor) class currently in use at CS as of 2024.<ref>{{Cite magazine |last=Bengtson |first=Kristian von |title=Bi-Liquid Success at Copenhagen Suborbitals |url=https://www.wired.com/2012/05/bi-liquid-success-at-copenhagen-suborbitals/ |access-date=2024-02-09 |magazine=Wired |language=en-US |issn=1059-1028}}</ref> |
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===HATV=== |
===HATV=== |
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[[File:Hatv guidance 320.jpg|thumb|Static test of the HATV at Refshaleøen 2011]] |
The HATV (Hybrid Atmospheric Test Vehicle) was a planned sounding rocket. The HATV booster was successfully static fired, though it was never launched.<ref>{{Citation |title=HATV Test 2011-10-22 Burn |url=https://www.youtube.com/watch?v=WdbP4XzKnkQ |access-date=2024-02-09 |language=en}}</ref> [[File:Hatv guidance 320.jpg|thumb|Static test of the HATV at Refshaleøen 2011]] |
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The HATV (Hybrid Atmospheric Test Vehicle) was a 220 mm diameter hybrid booster, used for testing purposes, it is one third the size of the HEAT rocket. It produces approximately 12 kN thrust within a combustion time of 20 seconds.{{citation needed|date=November 2011}} |
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===HEAT-1X=== |
===HEAT-1X=== |
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{{Main|HEAT 1X Tycho Brahe}} |
{{Main|HEAT 1X Tycho Brahe}} |
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HEAT 1X (''Hybrid Exo Atmospheric Transporter'')<ref name="SC">{{cite web|url=https://copenhagensuborbitals.com/spacecraft.php|title=Spacecraft|publisher=Copenhagen Suborbitals| |
HEAT 1X (''Hybrid Exo Atmospheric Transporter'')<ref name="SC">{{cite web|url=https://copenhagensuborbitals.com/spacecraft.php|title=Spacecraft|publisher=Copenhagen Suborbitals|access-date=8 September 2010|archive-url=https://web.archive.org/web/20100906003612/http://www.copenhagensuborbitals.com/spacecraft.php|archive-date=6 September 2010|url-status=dead}}</ref> was the [[Launch vehicle|rocket booster module]] intended to launch the space capsule ''Tycho Brahe'' into space, the combination being known as [[HEAT 1X Tycho Brahe|HEAT-1X TYCHO BRAHE]]. The rocket design was the result of numerous static-booster tests of the solid fuel [[resin|epoxy]] and the liquid oxidizer [[nitrous oxide]]. A combination which was also used in the scale-down test rocket HATV (''Hybrid Atmospheric Test Vehicle'') which was only one third the size of the HEAT. Stabilization of the rocket was provided through [[rolleron]]s. The rocket was launched on June 3rd, 2011. from the floating ''Sputnik'' platform.<ref>{{Cite web |title=HEAT-1X – Copenhagen Suborbitals |url=https://copenhagensuborbitals.com/missions/heat-1x/ |access-date=2024-02-10 |language=en-US}}</ref> |
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The rocket design was the result of numerous static-booster tests of the solid fuel [[resin|epoxy]] and the liquid oxidizer [[nitrous oxide]]. A combination which was also used in the scale-down test rocket HATV (''Hybrid Atmospheric Test Vehicle'') which was only one third the size of the HEAT. |
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Stabilization of the rocket was by [[rolleron]]s, a mechanism also used to stabilize missiles. The rocket was successfully launched 3 June 2011 but the test was aborted at an altitude of 2.8 km. |
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Within the first few seconds the rocket unexpectedly began to pitch over to approximately 30 degrees to horizontal. Due to the undesirable angle, the motor was manually commanded to shut down 16 seconds into flight at an altitude of 1.4 kilometers, with the rocket eventually rising to an apogee of approximately 2.8 kilometers, significantly off from the 30km goal.<ref name=":2">{{Cite web |date=2011-06-09 |title=Raketdukken Randy tog 26 G ved "landing" på havet {{!}} Ingeniøren |url=http://ing.dk/artikel/119815-raketdukken-randy-tog-26-g-ved-landing-paa-havet |access-date=2024-02-09 |archive-url=https://web.archive.org/web/20110609091215/http://ing.dk/artikel/119815-raketdukken-randy-tog-26-g-ved-landing-paa-havet |archive-date=2011-06-09 }}</ref> The rocket landed 8.5 kilometers<ref>{{Cite web |date=2011-06-05 |title=Raketten fløj, styrtede og samlede værdifuld data ind {{!}} Ingeniøren |url=http://ing.dk/artikel/119777-raketten-floej-styrtede-og-samlede-vaerdifuld-data-ind |access-date=2024-02-09 |archive-url=https://web.archive.org/web/20110605203341/http://ing.dk/artikel/119777-raketten-floej-styrtede-og-samlede-vaerdifuld-data-ind |archive-date=2011-06-05 }}</ref> away from the position where it was launched. The ''Tycho Brahe'' successfully separated from the booster, however, both the parachutes for the booster and ''Tycho Brahe'' did not successfully deploy. In the case of the ''Tycho Brahe'', it was successfully recovered from the ocean after suffering a 26G impact upon landing.<ref name=":2" /> It was found waterlogged and partially damaged. The booster sank to a depth of 80-90 meters. |
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[[File:HEATX1TychoBrahe.png|left|thumb|Drawing of the stacked rocket, with HEAT at the bottom. Compared with the final rocket]] |
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[[File:HEATX1TychoBrahe.png|left|thumb|Drawing of the stacked rocket, with HEAT at the bottom. Compared with the final rocket|369x369px]] |
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===TM-65 and TM-65 IIA and TM-65 IIB=== |
===TM-65 and TM-65 IIA and TM-65 IIB=== |
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{{Main|TM65}} |
{{Main|TM65}} |
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TM-65 and TM6-5 IIA/B were [[Liquid-propellant rocket|liquid propellant engine]]s using 75% [[Ethanol]] and liquid oxygen (LOX) as [[oxidizer]]. These engines produced about 65 kN thrust.<ref>{{cite web|title=TM65 Liquid propellant rocket engine|url=https://copenhagensuborbitals.com/tm65.php| |
TM-65 and TM6-5 IIA/B were [[Liquid-propellant rocket|liquid propellant engine]]s using 75% [[Ethanol]] and liquid oxygen (LOX) as [[oxidizer]]. These engines produced about 65 kN thrust.<ref>{{cite web|title=TM65 Liquid propellant rocket engine|url=https://copenhagensuborbitals.com/tm65.php|access-date=17 May 2012|archive-url=https://web.archive.org/web/20120516230854/http://www.copenhagensuborbitals.com/tm65.php|archive-date=16 May 2012|url-status=dead}}</ref> First static tests were conducted in May 2012. One TM65 II engine was for HEAT-2X and one was for HEAT-1600 LE. The TM-65 engine passed the test undamaged, and was fired at up to 50% of its rated thrust. The group planned to repeat the test with higher thrust levels, until the TM-65 class in 2014 was abandoned in favour of the BPM-100 engine concept.<ref>{{cite web|title=En stor dag for suborbitals.|url=http://ing.dk/artikel/129424-en-stor-dag-for-suborbitals|access-date=21 May 2012|archive-url=https://web.archive.org/web/20120523170132/http://ing.dk/artikel/129424-en-stor-dag-for-suborbitals|archive-date=23 May 2012|url-status=dead}}</ref> |
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===HEAT-2X=== |
===HEAT-2X=== |
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The HEAT-2X was a rocket built for flight-testing the TM-65 engine. It was planned to carry a 1:3 scale, 80 kg space capsule mock-up |
The HEAT-2X was a rocket built for flight-testing the TM-65 engine. It was planned to carry a 1:3 scale, 80 kg space capsule mock-up called the TDS-80 into the stratosphere above the [[Kármán line|Kárman Line]].<ref name=":5">{{Cite web |title=HEAT-2X – Copenhagen Suborbitals |url=https://copenhagensuborbitals.com/missions/heat-2x/ |access-date=2024-02-10 |language=en-US}}</ref> |
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The rocket was not flown as it suffered an engine fire during a static test in the summer of 2014. The rocket nozzle imploded and a welding seam opened resulting in the expulsion of all the ethanol fuel (some 500 L) in just three seconds resulting in a large fire which damaged |
The rocket was not flown as it suffered an engine fire during a static test in the summer of 2014.<ref name=":5" /> The rocket nozzle imploded and a welding seam opened resulting in the expulsion of all the ethanol fuel (some 500 L) in just three seconds resulting in a large fire which damaged part of the rocket. The engine failure and subsequent fire was filmed<ref name="Youtube">{{Citation |title=GoPro Just 3 feet Away From a Rocket Engine Explosion - HEAT-2X Rocket Static Fire |url=https://www.youtube.com/watch?v=f-4n-2MtECE |language=en}}</ref> up close with a high-speed camera, which although burned on the outside, survived the inferno enough for the film to be recovered. The fire damaged the onboard TM-65 engine enough to be unrepairable, leading to both the engine and HEAT-2X as a whole being retired to the CS museum.<ref>{{Cite web |title=HEAT-2X – Copenhagen Suborbitals |url=https://copenhagensuborbitals.com/missions/heat-2x/ |access-date=2024-02-09 |language=en-US}}</ref> This was one of the major deciding factors in choosing to retire the TM-65 class. |
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The engine failure and subsequent fire was filmed<ref name="Youtube">[https://www.youtube.com/watch?v=f-4n-2MtECE] Gopro Hero 3 camera</ref> up close with a high-speed camera, which although burned on the outside, survived the inferno enough for the film to be recovered. |
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=== |
=== RC-A1 Rocket and Recruits Initiative === |
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The Recruits Initiative, launched in 2021, was designed to attract and educate talented young individuals in the fields of rocket science and technology. The initiative also aimed at enhancing Danish expertise within the space and defense industries by fostering the development of skilled professionals. This project contributes to the success of the Spica project and it also strengthens the competitiveness of Danish businesses in the growing global space industry. |
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The HEAT-1600 LE and HEAT-1600 (after the 1600 mm diameter of the rockets), were the biggest rocket concept by the group, and was in pre-production in 2013. However, the 1600 mm diameter rocket and capsule concept was abandoned in 2014, in favour of the 950 mm diameter Spica rocket and capsule. HEAT-1600 LE was to be a full size version of the HEAT-1600 with only one TM-65 engine. The HEAT-1600 was planned to fly with a single 260 kN engine or a cluster of 4 x TM-65 engines fed by turbo pumps on a single stage.<ref>{{cite web | url=https://www.wired.com/wiredscience/2013/05/heat-1600-concept-development-the-manifestation-of-dreams-and-ambitions-for-download/ | title=HEAT 1600 Concept Development – The Manifestation of Dreams and Ambitions (for Download) | publisher=wired.com | date=2013-05-11 | accessdate=2013-05-12 | author=Von Bengtson, Kristian}}</ref> |
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The Recruit Rocket is a single-stage rocket designed and developed by the recruits team at Copenhagen Suborbitals. The rocket measures 5 meters in length from nose to engine, with a total weight, including fuel, of approximately 165 kg. Instead of a turbopump, it is powered by a dynamic pressure-regulating system (DPR). The BPM5 engine has been refined to the maximum during the rocket’s development, and through optimizing the design, it has achieved an impressive performance of 10 kN. The rocket’s top speed with a 5 kN motor is estimated to be 475 m/s, which is 1710 km/h. The project has provided a unique opportunity for the new members to gain hands-on experience, not only with the fundamental aspects of rocket design but also equipping them with the ability to tackle the various challenges that arise during rocket projects. As of 2024, the rocket is set for static testing in early 2025.<ref>{{Cite web |last=Wilson |first=Mads |date=2023-02-06 |title=Progress on the CS recruits rocket – Copenhagen Suborbitals |url=https://copenhagensuborbitals.com/progress-on-the-cs-recruits-rocket/?lang=da |access-date=2024-09-28 |language=da-DK}}</ref> |
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== Space capsules == |
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== |
==Space Capsules== |
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===Tycho Brahe=== |
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{{Main|HEAT 1X Tycho Brahe}} |
{{Main|HEAT 1X Tycho Brahe}} |
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{{multiple image|align=right |
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{{Double image|right|Rocket tacking02.jpg|{{#expr: (150 * (700 / 504)) round 0}}|Tycho Sketch.jpg|{{#expr: (150 * (2848 / 4272)) round 0}}|Tycho Brahe being stacked.|Sketch of the Tycho interior}} |
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| image1 = Rocket tacking02.jpg |
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The micro space craft (MSC), named [[Tycho Brahe]] after the Danish [[astronomer]], has a steel pressure hull, with room for one passenger. The passenger would be able to view the outside through a [[Poly(methyl methacrylate)|Perspex]] dome.<ref name="SC"/> The occupant would fly in a half-standing/half-sitting position, in a specially designed seat, and wearing [[G-suit|anti-G trousers]] to avoid [[G-LOC|blackout]]. Another compartment contains both the high-speed drogue parachute and the low-speed main parachutes for deceleration. The sheer volume of the MSC will provide the [[buoyancy]] in the water upon touchdown. |
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| width1 = {{#expr: (150 * (700 / 504)) round 0}} |
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| caption1 = Tycho Brahe being stacked. |
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| image2 = Tycho Sketch.jpg |
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| width2 = {{#expr: (150 * (2848 / 4272)) round 0}} |
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| caption2 = Sketch of the Tycho interior |
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}} |
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The micro space craft (MSC), named [[Tycho Brahe]] after the Danish [[astronomer]], has a steel pressure hull with room for one passenger.<ref>{{Cite web |date=2010-09-06 |title=C O P E N H A G E N S U B O R B I T A L S |url=http://www.copenhagensuborbitals.com/spacecraft.php |access-date=2024-01-09 |archive-url=https://web.archive.org/web/20100906003612/http://www.copenhagensuborbitals.com/spacecraft.php |archive-date=2010-09-06 }}</ref> |
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The passenger would be able to view the outside through a [[Poly(methyl methacrylate)|Perspex]] dome.<ref name="SC"/> The occupant would fly in a half-standing, half-sitting position in a specially designed seat and would be wearing [[G-suit|anti-G trousers]] to avoid [[G-LOC|blackout]]. Another compartment contains both the high-speed drogue parachute and the low-speed main parachutes for deceleration. The volume of the MSC will provide the [[buoyancy]] in the water upon touchdown.<ref name=":6">{{Cite web |date=June 3, 2011 |title=Copenhagen Suborbitals Flight Report - Heat-1X / Tycho Brahe |url=https://copenhagensuborbitals.com/wp_blog/wp_content/uploads/2013/11/HEAT1X_flight.pdf |access-date=February 9, 2024 |website=Copenhagen Suborbitals}}</ref> |
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The first MSC was christened "Tycho Brahe 1" and its first flight was uncrewed using a [[crash test dummy]].<ref>{{cite web | url=http://news.softpedia.com/news/Danish-Manned-Spacecraft-Built-by-Volunteers-153441.shtml | title=Danish Manned Spacecraft Built by Volunteers | author=Biliuti, Smaranda | publisher=Softpedia | date= 24 August 2010}}</ref> A new aluminium MSC called [[MAX-1 (Spacecraft)|MAX-1]] named after [[Maxime Faget]] is under development.{{citation needed|date=September 2012}} |
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According to the group, development on this capsule has been abandoned due to the physiological problems associated with rapid acceleration of a human in standing position.<ref>{{cite web | url=http://ing.dk/artikel/131361-store-nyheder-om-store-raketter | title=Store nyheder om store raketter | publisher=Ingeniøren | date=August 18, 2012 | accessdate=August 22, 2012 | author=Madsen Peter}}</ref> The craft is now on display in the [[Tycho Brahe Planetarium]] in Copenhagen.<ref>{{cite web|url=http://planetariet.dk/oplevelser/udstillingen/rumkapsel-landet-p%C3%A5-planetariet |title=Rumkapsel landet på planetariet |publisher=planetariet.dk |accessdate=September 30, 2012 |dead-url=yes |archiveurl=https://web.archive.org/web/20121109034516/http://planetariet.dk/oplevelser/udstillingen/rumkapsel-landet-p%C3%A5-planetariet |archivedate=November 9, 2012 }}</ref> |
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The first MSC was christened "Tycho Brahe 1" and its first flight was not crewed, instead using a [[crash test dummy]].<ref>{{cite web |url=http://news.softpedia.com/news/Danish-Manned-Spacecraft-Built-by-Volunteers-153441.shtml |title=Danish Manned Spacecraft Built by Volunteers |author=Biliuti, Smaranda |publisher=Softpedia |date= 24 August 2010}}</ref> A new aluminum MSC called [[MAX-1 (Spacecraft)|MAX-1]] named after [[Maxime Faget]] was under development but has been abandoned, according to the group, due to the physiological problems associated with rapid acceleration of a human in standing position.<ref>{{cite news |url=http://ing.dk/artikel/131361-store-nyheder-om-store-raketter |title=Store nyheder om store raketter |newspaper=Ingeniøren |date=August 18, 2012 |access-date=February 27, 2021 |author=Madsen Peter |archive-url=https://web.archive.org/web/20120821091839/http://ing.dk/artikel/131361-store-nyheder-om-store-raketter |archive-date=August 21, 2012 |url-status=dead}}</ref> The craft is now on display in the [[Tycho Brahe Planetarium]] in Copenhagen.<ref>{{cite web|url=http://planetariet.dk/oplevelser/udstillingen/rumkapsel-landet-p%C3%A5-planetariet |title=Rumkapsel landet på planetariet |publisher=planetariet.dk |access-date=September 30, 2012 |url-status=dead |archive-url=https://web.archive.org/web/20121109034516/http://planetariet.dk/oplevelser/udstillingen/rumkapsel-landet-p%C3%A5-planetariet |archive-date=November 9, 2012}}</ref> |
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=== Tycho Deep Space === |
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===Tycho Deep Space=== |
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[[File:TychoDeepSpaceAndLaunchEscapeSystem.jpg|thumbnail|left|Tycho Deep Space during testing of the Launch Escape System]] |
[[File:TychoDeepSpaceAndLaunchEscapeSystem.jpg|thumbnail|left|Tycho Deep Space during testing of the Launch Escape System]] |
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''Tycho Deep Space'' is a space capsule developed by [[Kristian |
''Tycho Deep Space'' is a space capsule developed by [[Kristian von Bengtson]].<ref name="copenhagensuborbitals.com">{{Cite web |title=Tycho Deep Space – Copenhagen Suborbitals |url=https://copenhagensuborbitals.com/missions/tycho-deep-space/ |access-date=2024-02-10 |language=en-US}}</ref> The first version officially named "Beautiful Betty" by [[Mikael Bertelsen]], the capsule's protector.<ref>{{cite web |url=https://copenhagensuborbitals.com/contentgfx/bertelsen_daab.jpg |title=Capsule protector Mikael Bertelsen naming the capsule |access-date=August 22, 2012 |author=Olsen, Jev |archive-url=https://web.archive.org/web/20121010134817/http://copenhagensuborbitals.com/contentgfx/bertelsen_daab.jpg |archive-date=October 10, 2012 |url-status=dead}}</ref> The uncrewed capsule was launched on 12 August 2012 at sea by a test [[Launch Escape System]], off the coast of [[Bornholm]]. The launch did not provide enough height for the parachute to deploy and the capsule was partly damaged on impact with the sea.<ref name="copenhagensuborbitals.com"/> Due to this damage, the TDS was retired. The capsule is 2 m in diameter, allowing for an astronaut to be in a horizontal position relative to the acceleration during launch and landing. This is in opposition to the first-generation Tycho Brahe design that required the astronaut to stand inside. |
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==Missions== |
==Missions== |
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The group originally focused on launching from a land based [[spaceport]] like [[Andøya Rocket Range|Andøya]], [[North European Aerospace Test range|Kiruna]], or [[Naval Air Station Keflavik|Iceland]]<ref>{{cite web|url=http://ing.dk/artikel/97766-ground-launch-site-den-onde-joker|title=Ground launch site - den onde joker|url-status=dead|access-date=11 August 2017|archive-date=11 June 2009|archive-url=https://web.archive.org/web/20090611151116/http://ing.dk/artikel/97766-ground-launch-site-den-onde-joker}}</ref> The focus then turned towards a sea launch just outside the [[Territorial waters#Territorial sea|territorial waters]] of Denmark. A permission to launch was given by Danish authorities, but the [[North Sea]], a possibility suggested by [[Danish Civil Aviation Administration]] (''Statens Luftfartsvæsen'') was rejected in 2009 by the [[Danish Maritime Authority]] (''Søfartsstyrelsen''). They preferred another area, giving formal and written permission to launch from the military [[firing range]] ESD138/ESD139,<ref>{{Cite web |title=About us – Copenhagen Suborbitals |url=https://copenhagensuborbitals.com/about-us/ |access-date=2024-02-10 |language=en-US}}</ref> located at {{Coord|55|02|57|N|15|36|11|E|region:DK|display=inline}} in the [[Baltic Sea]].{{citation needed|date=September 2012}} It is just outside [[Nexø]] on the Danish island of [[Bornholm]]. Copenhagen Suborbitals then had to build a floating [[mobile launcher platform]] (MLP) called ''[[Sputnik 1|Sputnik]]'', named after the first [[artificial satellite]] to be put into orbit. Their launch campaigns includes the following ships:{{citation needed|date=September 2012}} |
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* ''MLP-Sputnik'' - At first had to be towed via submarine,<ref>{{Cite web |last=Gallagher |first=Sean |date=2017-08-11 |title=Biggest amateur-built sub sinks—owner is suspected of killing passenger [Updated] |url=https://arstechnica.com/gadgets/2017/08/biggest-amateur-built-sub-sinks-owner-is-suspected-of-killing-passenger/ |access-date=2024-02-10 |website=Ars Technica |language=en-us}}</ref> but later it had two diesel engines installed,<ref>{{Cite web |title=Going to Space on an Homemade Rocket – |url=https://www.spacesafetymagazine.com/aerospace-engineering/rocketry/going-to-space-on-an-homemade-rocket/ |access-date=2024-02-10 |website=www.spacesafetymagazine.com}}</ref> and now sails under its own power. |
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The group originally focused on launching from a land based [[spaceport]] like [[Andøya Rocket Range|Andøya]], [[North European Aerospace Test range|Kiruna]] or [[Naval Air Station Keflavik|Iceland]]<ref>{{cite web|url=https://translate.google.com/translate?js=n&prev=_t&hl=en&ie=UTF-8&layout=2&eotf=1&sl=da&tl=en&u=http://ing.dk/artikel/97766-ground-launch-site-den-onde-joker&act=url|title=Google Translate|website=translate.google.com|accessdate=11 August 2017}}</ref> The focus however turned towards a sea launch, just outside the [[Territorial waters#Territorial sea|territorial waters]] of Denmark. A permission to launch was given by Danish authorities, but the first option, the [[North Sea]], a possibility suggested by [[Danish Civil Aviation Administration]] (''Statens Luftfartsvæsen''), was rejected in 2009 by the [[Danish Maritime Authority]] (''Søfartsstyrelsen''). They preferred another area and then gave a formal and written permission to launch from the military [[firing range]] ESD138/ESD139, which is located on the position {{Coord|55|02|57|N|15|36|11|E|region:DK|display=inline}} in the [[Baltic Sea]].{{citation needed|date=September 2012}} |
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* ''MHV Hjortø'' - A [[Home Guard (Denmark)#Naval Home Guard|Naval Home Guard]] vessel which serves as [[mission control]] and recovery vessel.<ref name=":6" /> |
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It is just outside [[Nexø]] on the Danish island of [[Bornholm]] and is therefore nicknamed Spaceport Nexø. The CS then had to build a floating [[mobile launcher platform]] (MLP), called ''Sputnik'' after [[Sputnik 1|the Russian spacecraft]] which was the first [[artificial satellite]] to be put into orbit. |
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Their launch campaigns includes the following ships:{{citation needed|date=September 2012}} |
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* ''MLP-Sputnik'', at first had to be towed, but later it had two diesel engines installed, and now sails under her own power. |
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* ''MHV Hjortø'', a [[Home Guard (Denmark)#Naval Home Guard|Naval Home Guard]] vessel which serves as [[mission control]] and recovery vessel. |
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* Two small [[rigid-hulled inflatable boat]]s. |
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===2010: The first launch attempt=== |
===2010: The first launch attempt=== |
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The first full-scale test-launch aimed at 30 km altitude was planned to be conducted off the coast of [[Bornholm]] between 30 August and 13 September 2010.<ref>[https://copenhagensuborbitals.com/campaignsep2010.php LAUNCH CAMPAIGN SEP 2010], Copenhagen Suborbitals</ref> The vehicle carried a [[crash test dummy]] "Rescue Randy" instead of a human pilot, with crewed flight not planned for some years. The success criteria were the completion of the sea voyage and countdown with launch |
The first full-scale test-launch aimed at 30 km altitude was planned to be conducted off the coast of [[Bornholm]] between 30 August and 13 September 2010.<ref>[https://copenhagensuborbitals.com/campaignsep2010.php LAUNCH CAMPAIGN SEP 2010] {{Webarchive|url=https://web.archive.org/web/20131021142215/http://www.copenhagensuborbitals.com/campaignsep2010.php |date=2013-10-21}}, Copenhagen Suborbitals</ref> The vehicle carried a [[crash test dummy]] "Rescue Randy"<ref>{{Cite magazine |last=Mosher |first=Dave |title=Watch Homemade Space Capsule Launch Livestream This Weekend |url=https://www.wired.com/2012/08/copenhagen-suborbitals-launch-escape-test/ |access-date=2024-02-10 |magazine=Wired |language=en-US |issn=1059-1028}}</ref> instead of a human pilot, with crewed flight not planned for some years. The success criteria were the completion of the sea voyage and a countdown with launch, with recovery planned as a bonus.<ref name="ing-criteria">{{cite web|last=Andersen|first=Kasper Brøndgaard|title=Experienced rocket builder doubts success (Danish)|url=http://ing.dk/artikel/111447-erfaren-raketbygger-tvivler-paa-succesfuld-dansk-opsendelse|publisher=Ing.dk|access-date=31 August 2010|archive-date=28 September 2011|archive-url=https://web.archive.org/web/20110928155227/http://ing.dk/artikel/111447-erfaren-raketbygger-tvivler-paa-succesfuld-dansk-opsendelse|url-status=dead}}</ref> |
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On Tuesday, 31 August 2010, the privately built Danish [[submarine]] [[UC3 Nautilus]] pushed the launch platform Sputnik carrying the rocket and spacecraft from Copenhagen towards the launch area near [[Nexø]], [[Bornholm]].<ref name="ingtow">{{cite web | |
On Tuesday, 31 August 2010, the privately built Danish [[submarine]] [[UC3 Nautilus]] pushed the launch platform Sputnik carrying the rocket and spacecraft from Copenhagen towards the launch area near [[Nexø]], [[Bornholm]].<ref name="ingtow">{{cite web |url=http://ing.dk/artikel/111523-nyt-fra-raket-holdet-vi-naar-nexoe-kl-2030 |title=Nyt fra raket-holdet: Vi når Nexø kl. 20.30 |publisher=ing.dk |date=1 September 2010 |access-date=1 September 2010 |author=Jensen, Mette Buck |archive-url=https://web.archive.org/web/20100903235244/http://ing.dk/artikel/111523-nyt-fra-raket-holdet-vi-naar-nexoe-kl-2030 |archive-date=3 September 2010 |url-status=dead}}</ref> |
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A launch attempt was made on Sunday, 5 September 2010, 14:43 [[Central European Summer Time|CEST]],<ref name=Ikke_i_luften>{{cite web|title=Raketten kom ikke i luften|url=http://ing.dk/artikel/111678-raketten-kom-ikke-i-luften|publisher=ing.dk| |
A launch attempt was made on Sunday, 5 September 2010, 14:43 [[Central European Summer Time|CEST]],<ref name="Ikke_i_luften">{{cite web|title=Raketten kom ikke i luften|url=http://ing.dk/artikel/111678-raketten-kom-ikke-i-luften|publisher=ing.dk|access-date=5 September 2010|archive-url=https://web.archive.org/web/20100908094712/http://ing.dk/artikel/111678-raketten-kom-ikke-i-luften|archive-date=8 September 2010|url-status=dead}}</ref> but the motor could not be started due to a failure of the [[liquid oxygen|LOX]] valve which is assumed to be caused by insufficient heating of the valve. The design famously included a consumer [[hair dryer]]<ref>{{Cite web |author1=Jeremy Hsu |date=2010-09-13 |title=Hair Dryer Glitch Pushes Private Danish Rocket Launch to 2011 |url=https://www.space.com/9113-hair-dryer-glitch-pushes-private-danish-rocket-launch-2011.html |access-date=2024-02-10 |website=Space.com |language=en}}</ref> for defrosting the LOX-valve; in effect it was not the blow-dryer but its power supply that failed.<ref name="ingnext2">{{cite web|last=Djursing|first=Thomas|title=Powerless hairdryer stopped rocket|url=http://ing.dk/artikel/111683-stroemsvigt-til-foetex-foentoerrer-stoppede-raket|publisher=ing.dk|access-date=5 September 2010|archive-url=https://web.archive.org/web/20100908182952/http://ing.dk/artikel/111683-stroemsvigt-til-foetex-foentoerrer-stoppede-raket|archive-date=8 September 2010|url-status=dead}}</ref> |
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The group promised to come back the year after to attempt the launch again.<ref>{{cite web | |
The group promised to come back the year after to attempt the launch again.<ref>{{cite web |url=http://ing.dk/artikel/111713-vi-er-stolte-vi-er-glade-vi-gir-aldrig-op |title=Vi er stolte - vi er glade - vi gir aldrig op...(Danish) |publisher=ing.dk |date=6 September 2010 |access-date=1 January 2012 |author=Kristian von Bengtson and Peter Madsen |archive-date=20 October 2012 |archive-url=https://web.archive.org/web/20121020044216/http://ing.dk/artikel/111713-vi-er-stolte-vi-er-glade-vi-gir-aldrig-op |url-status=dead}}</ref> |
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===2011: First flight of ''HEAT-1X Tycho Brahe''=== |
===2011: First flight of ''HEAT-1X Tycho Brahe''=== |
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[[File:20110603-1851.jpg|thumb|right|HEAT 1X Tycho Brahe lifting off from MLP-Sputnik]] |
[[File:20110603-1851.jpg|thumb|right|HEAT 1X Tycho Brahe lifting off from MLP-Sputnik]] |
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Having done updates on the rocket, and the valve, and with MLP-Sputnik under her own power, and a support vessel, the group sailed again for Spaceport Nexø on May 28 at 4:50 a.m. They again met up with [[Home Guard (Denmark)#Naval Home Guard|MHV Hjortø]], a Naval Home Guard vessel that serves as [[mission control]] and recovery vessel. |
Having done updates on the rocket, and the valve, and with MLP-Sputnik under her own power, and a support vessel, the group sailed again for Spaceport Nexø on May 28 at 4:50 a.m. They again met up with [[Home Guard (Denmark)#Naval Home Guard|MHV Hjortø]], a Naval Home Guard vessel that serves as [[mission control]] and recovery vessel. The second launch attempt was more successful and the maiden flight took place 3 June 2011,<ref name=":4" /> at 16:32 local time (CEST) (14:32 GMT). The HEAT-1X rocket lifted off, but was only able to ascend to an altitude of only 2.8 km.<ref>{{cite news|url=https://www.foxnews.com/science/danish-teams-homemade-space-capsule-blasts-off|title=Danish Team's Homemade Space Capsule Blasts Off|work=foxnews |date=3 June 2011}}</ref> Mission Control had to shut the engine off early after 21 seconds.<ref name="success-pol">{{cite news |url=http://politiken.dk/videnskab/ECE1299139/flyt-jer-lige-lidt-nasa-her-kommer-danmark/ |title=Flyt jer lige lidt, Nasa: Her kommer Danmark |publisher=Politiken |date=3 June 2011 |access-date=3 June 2011 |author=Astrup, Søren |author2=Lindqvist, Andreas |language=da |archive-url=https://web.archive.org/web/20110605025602/http://politiken.dk/videnskab/ECE1299139/flyt-jer-lige-lidt-nasa-her-kommer-danmark/ |archive-date=5 June 2011 |url-status=dead}}</ref> |
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The second launch attempt was more successful and the maiden flight took place 3 June 2011, at 16:32 local time (CEST) (14:32 GMT). The HEAT-1X rocket lifted off and ascended to an altitude of only 2.8 km,<ref>{{cite news|url=http://www.foxnews.com/scitech/2011/06/03/danish-teams-homemade-space-capsule-blasts-off/|title=Danish Team's Homemade Space Capsule Blasts Off|publisher=foxnews | date=3 June 2011}}</ref> because Mission Control had to shut the engine off after 21 seconds.<ref name="success-pol">{{cite news | url=http://politiken.dk/videnskab/ECE1299139/flyt-jer-lige-lidt-nasa-her-kommer-danmark/ | title=Flyt jer lige lidt, Nasa: Her kommer Danmark | publisher=Politiken | date=3 June 2011 | accessdate=3 June 2011 | author=Astrup, Søren | author2=Lindqvist, Andreas | language=Danish}}</ref> Although there were problems with the parachutes, the ''HEAT-1X Tycho Brahe'' was recovered and the flight produced useful data for subsequent development of the program. |
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== 2012 Missions == |
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=== SMARAGD Flight === |
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[[File:SmaragdHABCS.jpg|thumb|left|The two-stage Smaragd in the HAB, missing only electronics]] |
[[File:SmaragdHABCS.jpg|thumb|left|The two-stage Smaragd in the HAB, missing only electronics with Peter Madsen on the right side]] |
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The SMARAGD rocket (''[[emerald]]'' in [[Danish language|Danish]]) is a 5.7 meter<ref>{{cite news |url=http://ing.dk/tema/raket |title=Copenhagen suborbitals aktiviteter i 2012 |newspaper=Ingeniøren |access-date=September 2, 2012 |archive-url=https://web.archive.org/web/20110127032935/http://ing.dk/tema/raket |archive-date=January 27, 2011 |url-status=dead}}</ref> two-stage rocket weighing 160 kg, intended to reach an altitude in excess of 20km,<ref>{{Cite web |title=Smaragd – Copenhagen Suborbitals |url=https://copenhagensuborbitals.com/missions/smaragd/ |access-date=2024-02-10 |language=en-US}}</ref> that was used for testing various technological aspects of the operation. On July 27, 2012, the team set out from Nexø towards the launch site, intending to launch the SMARAGD rocket.<ref>{{cite web |url=http://ing.dk/artikel/130863-alle-skibe-er-paa-vej-mod-affyringsomraadet |title=Alle skibe er på vej mod affyringsområdet |publisher=www.ing.dk |access-date=27 July 2012 |author=Djursing, Thomas |archive-date=31 July 2012 |archive-url=https://web.archive.org/web/20120731061513/http://ing.dk/artikel/130863-alle-skibe-er-paa-vej-mod-affyringsomraadet |url-status=dead}}</ref><ref>{{cite web |url=http://ing.dk/artikel/130862-saa-staar-smaragd-skudklar-se-de-sidste-forberedelser-her |title=Så står Smaragd skudklar: Se de sidste forberedelser her |publisher=www.ing.dk |access-date=27 July 2012 |author=Djursing Thomas |archive-date=28 July 2012 |archive-url=https://web.archive.org/web/20120728051334/http://ing.dk/artikel/130862-saa-staar-smaragd-skudklar-se-de-sidste-forberedelser-her |url-status=dead}}</ref> After some initial problems with the remote launch control,<ref>{{cite web |url=http://ing.dk/artikel/130875-skuffelse-raket-affyrede-ikkemen-nyt-forsoeg-kl-1250 |title=Skuffelse: Raket affyrede ikke...men nyt forsøg kl. 12.50 |access-date=27 July 2012 |author=Djursing, Thomas |archive-date=30 July 2012 |archive-url=https://web.archive.org/web/20120730075901/http://ing.dk/artikel/130875-skuffelse-raket-affyrede-ikkemen-nyt-forsoeg-kl-1250 |url-status=dead}}</ref> the rocket launched successfully just after 1 pm<ref>{{cite web |url=http://ing.dk/artikel/130879-smaragd-er-i-luften |title=Smaragd er i luften |publisher=www.ing.dtu.dk |access-date=27 July 2012 |author=Stage, Mie |archive-url=https://web.archive.org/web/20120730052007/http://ing.dk/artikel/130879-smaragd-er-i-luften |archive-date=30 July 2012 |url-status=dead}}</ref><ref>{{cite web |url=http://politiken.dk/indland/ECE1701129/danske-amatoer-astronauter-har-sendt-en-ny-raket-af-sted-fra-nexoe/ |title=Danske amatør-astronauter har sendt en ny raket af sted fra Nexø |publisher=Politiken |date=27 July 2012 |access-date=August 6, 2012}}</ref> and reached a maximum altitude of 8.2 km.<ref name="h8.2">{{cite web|url = http://www.nyteknik.se/tidningen/article3512650.ece|title = Danes launch homemade rocket|publisher = [[Ny Teknik]]|date = 27 July 2012|access-date = 7 August 2012|author = Melzer, Jonas.|archive-date = 29 July 2012|archive-url = https://web.archive.org/web/20120729233152/http://www.nyteknik.se/tidningen/article3512650.ece|url-status = dead}}</ref> It was evident shortly after takeoff that the nosecone containing electronics broke off during launch, possibly due to the large acceleration of estimated 20 g.<ref>{{cite web |url=http://ing.dk/artikel/130607-naesekegle-broed-i-stykker-kort-efter-raketstart |title=Næsekegle brød i stykker kort efter raketstart |access-date=27 July 2012 |author=Djursing, Thomas |archive-date=30 July 2012 |archive-url=https://web.archive.org/web/20120730051957/http://ing.dk/artikel/130607-naesekegle-broed-i-stykker-kort-efter-raketstart |url-status=dead}}</ref> |
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=== Tycho Deep Space / LES flight === |
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The SMARAGD rocket (''[[emerald]]'' in Danish) is a 5.7 meter<ref>{{cite web | url=http://ing.dk/tema/raket | title=Copenhagen suborbitals aktiviteter i 2012 | publisher=Ingeniøren | accessdate=September 2, 2012}}</ref> two-stage rocket weighing 160 kg, intended to reach an altitude of 8 km,<ref>{{cite web | url=http://ing.dk/artikel/130850-smaragd-raketten-goeres-klar-nu-skal-cs-skyde-hoejtog-ligeud | title=Smaragd-raketten gøres klar: Nu skal CS skyde højt…og ligeud | publisher=www.ing.dk | accessdate=27 July 2012 | author=Djursing, Thomas}}</ref> that was used for testing various technological aspects of the operation. |
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On 12 August 2012 at 09:18, the space capsule Tycho Deep Space was launched to test a [[launch escape system]]. However the parachute did not deploy properly and the capsule was damaged on impact.<ref>{{cite web |url=http://ing.dk/artikel/131151-kapsel-er-haardt-medtaget-efter-fejlslagen-opsendelse |title=Kapsel er hårdt medtaget efter fejlslagen opsendelse |publisher=www.ing.dk |date=August 12, 2012 |access-date=August 12, 2012 |author=Djursing, Thomas |url-status=dead |archive-url=https://archive.today/20130212172902/http://ing.dk/artikel/131151-kapsel-er-haardt-medtaget-efter-fejlslagen-opsendelse |archive-date=February 12, 2013}}</ref> Several media had misunderstood the schedule and proclaimed the launch to have been started prematurely due to an error.<ref>{{cite web |url=http://politiken.dk/videnskab/ECE1718357/hov-hvad-skete-der-dansk-rumraket-roeg-pludselig-i-vejret/ |title=Hov, hvad skete der? Dansk rumraket røg pludselig i vejret : Den danske raket blev affyret tre kvarter, før den skulle. |publisher=www.politiken.dk |date=August 12, 2012 |access-date=August 12, 2012 |author=KROMANN, HANS CHRISTIAN |archive-url=https://web.archive.org/web/20120813194316/http://politiken.dk/videnskab/ECE1718357/hov-hvad-skete-der-dansk-rumraket-roeg-pludselig-i-vejret/ |archive-date=August 13, 2012 |url-status=dead}}</ref> The test was considered partly successful by the team, due to the successful rocket launch and the unsuccessful parachute deployment.<ref>{{cite news |url=http://ing.dk/artikel/131151-kapsel-haardt-medtaget-efter-for-lav-flyvning |title=Kapsel hårdt medtaget efter for lav flyvning |newspaper=Ingeniøren |date=August 12, 2012 |access-date=August 12, 2012 |author=Djursing, Thomas |archive-url=https://web.archive.org/web/20120813205302/http://ing.dk/artikel/131151-kapsel-haardt-medtaget-efter-for-lav-flyvning |archive-date=August 13, 2012 |url-status=dead}}</ref> The launch could be followed live via live streaming from several video cameras; additionally high-speed cameras were mounted on the MLP.<ref>{{cite video |url=https://www.youtube.com/watch?v=gNFh6zN0rGY&feature=player_embedded |archive-url=https://ghostarchive.org/varchive/youtube/20211215/gNFh6zN0rGY |archive-date=2021-12-15 |url-status=live| title=LES/TDS launch |publisher=Copenhagen Suborbitals}}{{cbignore}}</ref> |
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On July 27, 2012, the team set out from Nexø towards the launch site, intending to launch the SMARAGD rocket.<ref>{{cite web | url=http://ing.dk/artikel/130863-alle-skibe-er-paa-vej-mod-affyringsomraadet | title=Alle skibe er på vej mod affyringsområdet | publisher=www.ing.dk | accessdate=27 July 2012 | author=Djursing, Thomas}}</ref><ref>{{cite web | url=http://ing.dk/artikel/130862-saa-staar-smaragd-skudklar-se-de-sidste-forberedelser-her#0 | title=Så står Smaragd skudklar: Se de sidste forberedelser her | publisher=www.ing.dk | accessdate=27 July 2012 | author=Djursing Thomas}}</ref> After some initial problems with the remote launch control,<ref>{{cite web | url=http://ing.dk/artikel/130875-skuffelse-raket-affyrede-ikkemen-nyt-forsoeg-kl-1250 | title=Skuffelse: Raket affyrede ikke...men nyt forsøg kl. 12.50 | accessdate=27 July 2012 | author=Djursing, Thomas}}</ref> the rocket launched successfully just after 1 pm<ref>{{cite web | url=http://ing.dk/artikel/130879-smaragd-er-i-luften | title=Smaragd er i luften | publisher=www.ing.dtu.dk | accessdate=27 July 2012 | author=Stage, Mie}}</ref><ref>{{cite web | url=http://politiken.dk/indland/ECE1701129/danske-amatoer-astronauter-har-sendt-en-ny-raket-af-sted-fra-nexoe/ | title=Danske amatør-astronauter har sendt en ny raket af sted fra Nexø | publisher=Politiken | date=27 July 2012 | accessdate=August 6, 2012}}</ref> and reached the maximum altitude of 8.2 km.<ref name="h8.2">{{cite web |url = http://www.nyteknik.se/tidningen/article3512650.ece|title = Danes launch homemade rocket|publisher = ''[[Ny Teknik]]''|date = 27 July 2012|accessdate = 7 August 2012|author = Melzer, Jonas.}}</ref> It was evident shortly after take off that the nosecone, containing electronics, broke off during launch, possibly due to the large acceleration of estimated 20 g.<ref>{{cite web | url=http://ing.dk/artikel/130607-naesekegle-broed-i-stykker-kort-efter-raketstart | title=Næsekegle brød i stykker kort efter raketstart | accessdate=27 July 2012 | author=Djursing, Thomas}}</ref> |
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== 2013 Missions == |
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====Tycho Deep Space / LES flight==== |
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On 12 August 2012 at 09:18, the space capsule Tycho Deep Space, was launched to test a [[launch escape system]]. However the parachute did not deploy properly and the capsule was damaged on impact.<ref>{{cite web | url=http://ing.dk/artikel/131151-kapsel-er-haardt-medtaget-efter-fejlslagen-opsendelse | title=Kapsel er hårdt medtaget efter fejlslagen opsendelse | publisher=www.ing.dk | date=August 12, 2012 | accessdate=August 12, 2012 | author=Djursing, Thomas | deadurl=yes | archiveurl=https://archive.is/20130212172902/http://ing.dk/artikel/131151-kapsel-er-haardt-medtaget-efter-fejlslagen-opsendelse | archivedate=February 12, 2013 | df= }}</ref> Several media had misunderstood the schedule and proclaimed the launch to have been started prematurely due to an error.<ref>{{cite web | url=http://politiken.dk/videnskab/ECE1718357/hov-hvad-skete-der-dansk-rumraket-roeg-pludselig-i-vejret/ | title=Hov, hvad skete der? Dansk rumraket røg pludselig i vejret : Den danske raket blev affyret tre kvarter, før den skulle. | publisher=www.politiken.dk | date=August 12, 2012 | accessdate=August 12, 2012 | author=KROMANN, HANS CHRISTIAN}}</ref> The test was considered partly successful by the team, due to the successful rocket launch and the unsuccessful parachute deployment.<ref>{{cite web | url=http://ing.dk/artikel/131151-kapsel-haardt-medtaget-efter-for-lav-flyvning | title=Kapsel hårdt medtaget efter for lav flyvning | publisher=Ingeniøren | date=August 12, 2012 | accessdate=August 12, 2012 | author=Djursing, Thomas}}</ref> The launch could be followed live via live streaming from several video cameras, additionally high-speed cameras were mounted on the MLP.<ref>{{cite video | url=https://www.youtube.com/watch?v=gNFh6zN0rGY&feature=player_embedded | title=LES/TDS launch | publisher=Copenhagen Suborbitals}}</ref> |
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=== |
=== SAPPHIRE-1 Mission === |
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''SAPPHIRE-1'', a modification of the HATV, was a 4.5 m rocket whose main purpose was to test the [[Guidance system|active guidance system]] developed by Copenhagen Suborbitals.<ref>{{cite web |url=http://ing.dk/artikel/130956-katapultsaede-til-dansk-rumkapsel-skydes-op-til-12-kilometer-om-faa-dage |title=Ejection seat soon to launch |access-date=2 August 2012 |author=Djursing, Thomas |archive-url=https://web.archive.org/web/20120804212745/http://ing.dk/artikel/130956-katapultsaede-til-dansk-rumkapsel-skydes-op-til-12-kilometer-om-faa-dage |archive-date=4 August 2012 |url-status=dead}}</ref> It was successfully launched on 23 June 2013.<ref>{{cite web|url=http://ing.dk/artikel/kaempe-succes-raket-floej-lodret-til-over-otte-kilometer-159938|archive-url=https://archive.today/20130624233603/http://ing.dk/artikel/kaempe-succes-raket-floej-lodret-til-over-otte-kilometer-159938|url-status=dead|archive-date=June 24, 2013|title=Kæmpe succes: Raket fløj lodret over otte kilometer - Ingeniøren|date=23 June 2013|website=Ing.dk|access-date=11 August 2017}}</ref> |
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== 2016 Missions == |
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====SAPPHIRE-1 Mission==== |
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''SAPPHIRE-1'', a modification of the HATV, was a 4.5m rocket whose main purpose was to test the [[Guidance system|active guidance system]] developed by Copenhagen Suborbitals.<ref>{{cite web | url=http://ing.dk/artikel/130956-katapultsaede-til-dansk-rumkapsel-skydes-op-til-12-kilometer-om-faa-dage | title=Ejection seat soon to launch | accessdate=2 August 2012 | author=Djursing, Thomas}}</ref> It was successfully launched on 23 June 2013.<ref>{{cite web|url=http://ing.dk/artikel/kaempe-succes-raket-floej-lodret-til-over-otte-kilometer-159938|title=Kæmpe succes: Raket fløj lodret over otte kilometer - Ingeniøren|date=23 June 2013|website=Ing.dk|accessdate=11 August 2017}}</ref> |
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===Nexø I=== |
===Nexø I=== |
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Nexø I was launched Saturday, 23 July 2016, with inaugural BPM-5 engine. It was a partial success |
Nexø I was launched Saturday, 23 July 2016, with inaugural BPM-5 engine. It was a partial success, and the supply of liquid oxygen to the engine was insufficient due to partial premature evaporation.<ref>{{cite web|url=https://copenhagensuborbitals.com/roadmap/nexo-i|title=Nexø I – Copenhagen Suborbitals|website=Copenhagensuborbitals.com|access-date=25 April 2018}}</ref><ref name=nex>{{cite web|url=https://copenhagensuborbitals.com/nexo|title=Nexø 1 Guidance Navigation & Control – Copenhagen Suborbitals|website=Copenhagensuborbitals.com|date=30 July 2016 |access-date=25 April 2018}}</ref> |
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== 2018 Missions == |
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===Nexø II=== |
===Nexø II=== |
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The Nexø II was successfully launched on 4 August 2018, with a slightly modified BPM-5 engine. It reached an apogee of 8–12 km and was safely recovered via parachute.<ref>{{cite web |title=The full story of the Nexø II mission |url=https://www.youtube.com/watch?v=BVwTU7FXmGE |archive-url=https://ghostarchive.org/varchive/youtube/20211215/BVwTU7FXmGE |archive-date=2021-12-15 |url-status=live|publisher=Copenhagen Suborbitals |access-date=11 June 2020}}{{cbignore}}</ref> |
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The preparation of the launch of Nexø II is ongoing. However, as of April 2018, the rocket didn't get off the ground this year due to NoGo from the Swedish air traffic control. It launched on 4 August 2018, with slightly modified BPM-5 engine.<ref name=nex /> |
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==Goals and records achieved== |
==Goals and records achieved== |
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Copenhagen Suborbitals' achievements include: |
Copenhagen Suborbitals' achievements include: |
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* Most powerful amateur rocket ever flown.<ref>{{Cite web |last=Motherboard |first=Xavier Aaronson / |date=2012-12-21 |title=Open Source Outer Space: How A Couple Of Guys Are Building A Homemade Rocket Ship for the Masses |url=https://www.popsci.com/technology/article/2012-12/open-source-outer-space-how-couple-guys-are-building-homemade-rocket-ship-masses/ |access-date=2024-02-10 |website=Popular Science |language=en-US}}</ref> |
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* Most powerful amateur rocket ever flown. |
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* First amateur rocket flown with a payload of a full-size [[crash test dummy]]. |
* First amateur rocket flown with a payload of a full-size [[crash test dummy]].<ref>{{Cite web |date=2011-07-07 |title=Amateur Rocket Launch |url=https://www.flyingmag.com/photo-gallery-photos-amateur-rocket-launch/ |access-date=2024-02-10 |website=FLYING Magazine |language=en-US}}</ref> |
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* First |
* First Main Engine(s) Cut-Off (MECO) command sent to, received and performed by an amateur rocket.<ref>{{Cite news |last=Clayton |first=Nick |title=Building an Open-Source Manned Space Rocket in Denmark |url=https://www.wsj.com/articles/BL-TEB-5052 |access-date=2024-02-10 |work=WSJ |language=en-US}}</ref> |
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* Handling and orchestration of a sea launch |
* Handling and orchestration of a sea launch by a small-budget organization.<ref>{{Cite web |title=Copenhagen Suborbitals: Low Budget Rocketeers - Go Denmark! - blog - AirPigz |url=http://airpigz.com/blog/2010/8/25/copenhagen-suborbitals-low-budget-rocketeers-go-denmark.html |access-date=2024-02-10 |website=airpigz.com |language=en}}</ref> |
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On 3 October 2013, Copenhagen Suborbitals was awarded the "Breitling Milestone Trophy" award by [[Fédération Aéronautique Internationale]] at a ceremony in [[Kuala Lumpur]].<ref>{{cite web|url=http://www.fai.org/news/37886-2013-fai-awards-ceremony|title=2013 FAI Awards Ceremony|first=Faustine|last=Carrera|website=Fai.org| |
On 3 October 2013, Copenhagen Suborbitals was awarded the "Breitling Milestone Trophy" award by [[Fédération Aéronautique Internationale]] at a ceremony in [[Kuala Lumpur]].<ref>{{cite web|url=http://www.fai.org/news/37886-2013-fai-awards-ceremony|title=2013 FAI Awards Ceremony|first=Faustine|last=Carrera|website=Fai.org|access-date=11 August 2017}}</ref><ref>Søren Munch. "[http://jyllands-posten.dk/indland/ECE6061373/rakettur-pa-8-km-beloennet-med-fornem-pris?ref=lokalavisen Rakettur på 8 km belønnet med fornem pris] {{webarchive|url=https://web.archive.org/web/20150611004618/http://jyllands-posten.dk/indland/ECE6061373/rakettur-pa-8-km-beloennet-med-fornem-pris?ref=lokalavisen |date=2015-06-11}}" ''[[Jyllands-Posten]]'', 7 October 2013. Accessed: 7 October 2013.</ref> |
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==Support group== |
==Support group== |
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In 2010, an independent group of space enthusiasts founded the Copenhagen Suborbitals Support group (CSS).<ref name=":7">{{Cite web |title=Support Us – Copenhagen Suborbitals |url=https://copenhagensuborbitals.com/support-us/ |access-date=2024-02-10 |language=en-US}}</ref> The main purpose of this group is to "support CS economically, morally and practically in their mission". Within two days after its founding, CSS reached 100 members. November 15, 2011 marked a major milestone for CSS as 500 members was reached. As of early 2024, around 600 members were recorded.<ref name=":7" /> |
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By paying a fixed monthly amount, the members of Copenhagen Suborbitals Support now |
By paying a fixed monthly amount, the members of Copenhagen Suborbitals Support now cover most of the fixed costs for the project in addition to donating various forms of hardware.<ref name="raketvenner">{{cite web |url=http://rocketfriends.org/ |title=The official Copenhagen Suborbitals support group |publisher=Copenhagen Suborbitals Support |access-date=5 March 2013 |archive-url=https://web.archive.org/web/20120816070910/http://rocketfriends.org/ |archive-date=16 August 2012 |url-status=dead}}</ref> By 2015, CS was supported with {{£|12,500}} per month.<ref>Smith, Julian. "[https://www.wired.co.uk/article/diy-space How the final frontier just got democratised]". ''[[Wired (magazine)|Wired]]'', 20 May 2015. [https://web.archive.org/web/20150525152643/http://www.wired.co.uk/magazine/archive/2015/06/features/diy-space/page/6 Archived] on 25 May 2015.</ref> |
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==References== |
==References== |
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==External links== |
==External links== |
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{{Commons|Copenhagen_Suborbitals|Copenhagen Suborbitals}} |
{{Commons|Copenhagen_Suborbitals|Copenhagen Suborbitals}} |
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{{ |
{{external media|float=right|width=330px |
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| image1 =[https://picasaweb.google.com/114657365514543526210 Picasa Web album (many Wikipedia compatible licences)] |
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|align=right|width=330px |
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| image1 =[https://picasaweb.google.com/114657365514543526210 Picasa Web album (many wikipedia compatible licences)] |
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| video1 ={{YouTube|id=K7YZpvs513U|title= HEAT1X-Tycho launch highlights}} |
| video1 ={{YouTube|id=K7YZpvs513U|title= HEAT1X-Tycho launch highlights}} |
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| video2 =[http://tedxtalks.ted.com/video/TEDxCopenhagen-Kristian-von-Ben/ Lecture by Kristian von Bengtson] on [[TED (conference)#Other programs|TEDx]] |
| video2 =[http://tedxtalks.ted.com/video/TEDxCopenhagen-Kristian-von-Ben/ Lecture by Kristian von Bengtson] on [[TED (conference)#Other programs|TEDx]] |
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* [https://copenhagensuborbitals.com/ Copenhagen Suborbitals] official website |
* [https://copenhagensuborbitals.com/ Copenhagen Suborbitals] official website |
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* [https://www.wired.com/wiredscience/rocketshop/ Wired blog] written by Kristian von Bengtson of Copenhagen Suborbitals |
* [https://www.wired.com/wiredscience/rocketshop/ Wired blog] written by Kristian von Bengtson of Copenhagen Suborbitals |
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* [http://ing.dk/tema/raket Project overview] on [[Ingeniøren]] |
* [https://web.archive.org/web/20110127032935/http://ing.dk/tema/raket Project overview] on [[Ingeniøren]] |
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* [http://ing.dk/blogs/rumfart-pa-den-anden-made Danish blog] written by the people of Copenhagen Suborbitals |
* [http://ing.dk/blogs/rumfart-pa-den-anden-made Danish blog] written by the people of Copenhagen Suborbitals |
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{{Spaceflight}} |
{{Spaceflight}} |
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[[Category:Copenhagen Suborbitals| ]] |
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[[Category:Technology companies established in 2008]] |
[[Category:Technology companies established in 2008]] |
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[[Category:Non-profit organizations based in Denmark]] |
[[Category:Non-profit organizations based in Denmark]] |
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[[Category:Organizations based in Copenhagen]] |
[[Category:Organizations based in Copenhagen]] |
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[[Category:Private spaceflight companies]] |
[[Category:Private spaceflight companies]] |
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[[Category:Rocket engine manufacturers]] |
[[Category:Rocket engine manufacturers of Denmark]] |
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[[Category:Open-source hardware]] |
[[Category:Open-source hardware]] |
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[[Category:Suborbital spaceflight]] |
[[Category:Suborbital spaceflight]] |
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[[Category:2008 establishments in Denmark]] |
[[Category:2008 establishments in Denmark]] |
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[[Category: |
[[Category:Amateur crewed rocketry]] |
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[[Category:Peter Madsen]] |
Latest revision as of 23:34, 9 November 2024
Company type | Non-profit, open source, amateur, all-volunteer organisation |
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Industry | Aerospace |
Founded | 1 May 2008 |
Founders | Kristian von Bengtson Peter Madsen |
Headquarters | Refshaleøen, Copenhagen, Denmark 55°41′29.1″N 12°37′1.21″E / 55.691417°N 12.6170028°E |
Key people | Chairman: Jørgen Skyt Vice Chairman: Storm Boysen Executive Officer: Niels Johansen Communication Director: Mads Wilson Space Strategist: Thomas Pedersen Space medicine: Niels Foldager |
Number of employees | 55[1] (all volunteering)[2] |
Website | copenhagensuborbitals |
Part of a series on |
Private spaceflight |
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Active companies |
Active vehicles |
Contracts and programs |
Related |
Copenhagen Suborbitals is a crowd-funded human space program. It has flown six home-built rockets and capsules since 2011.[3] The organization successfully launched its Nexø II rocket in the summer of 2018.[4][5] Its stated goal is to have one of its members reach space (above 100 km) on a sub-orbital spaceflight. The organization was founded by Kristian von Bengtson and Peter Madsen.[6]
As of September 2024, the program has 63 volunteers who elect a chairman and board members at their annual general assemblies. The chairman is Jørgen Skyt.
History
[edit]Copenhagen Suborbitals was founded in 2008 by Kristian von Bengtson and Peter Madsen as a non-profit, crowd-funded project that discussed most of their operations on blogs[7][8] and lectures.[9]
On 23 February 2014, the board of Copenhagen Suborbitals announced that Kristian von Bengtson had left the group, after falling out with Madsen. Madsen left in June 2014.[10]
Rockets and engines
[edit]Spica
[edit]In 2014, Copenhagen Suborbitals designed a basic first crewed rocket and space capsule. They named it Spica, and it is planned to stand 12–14 m tall with a diameter of 950 mm.[11] As of late September 2024, two pressure hardened 950mm steel tanks have been constructed and the development of the BPM-25 engine class is well underway.
Originally, the Spica rocket was planned to be powered by the BPM-100 class, but due to internal manufacturing troubles, the BPM-25 was eventually decided on as the engine to power the rocket.[12] Though it is weaker, it provides several advantages through greater roll authority and flow control. The BPM-25 engines, unlike the BPM-100, will have to be clustered in order to achieve the necessary thrust to launch Spica to the desired altitude. The BPM-25 provides 25 kN of thrust.[13] Similar to the BPM-100 engine, it uses liquid oxygen as oxidizer and ethanol as fuel. Spica will maneuver by thrust vectoring on its BPM-25 engines.
The rocket will be fully guided by home-built electronics and software. Many of the systems and technology planned for use on this rocket were previously tested and proven on the smaller Nexø class rockets in during the 2016 to 2018 period.[14] The space capsule will be of a tubular design similar to its predecessor Tycho Brahe. While the Spica capsule has not entered more than marginal construction as of 2024, CS plans on first building a boilerplate capsule to test on the ground before moving onto the real article.[15]
BPM-2 and BPM-5
[edit]During the 2016-2018 period, the group designed, built and tested a series of smaller engines with a nominal thrust of 2 and 5 kN - the BPM(Bi-Propellant Motor)-2 class and BPM-5 class respectively. Nexø I launched under the power of a BPM-5 on July 23rd, 2016.[16] On August 4, 2018, just as the Nexø I, Nexø II was launched under the power of a BPM-5.[14] The Nexø class was primarily intended to serve as a technology demonstrator ahead of the development of Spica.[14] The BPM engines are bi-liquid rocket engines using LOX and ethanol, regeneratively cooled by the ethanol fuel.[17]
The BPM-2 was primarily intended to serve as a test article for the CS test stand and manufacturing methods, and was never intended to launch a rocket. The BPM-2 engine was static fired 4 separate times on May 2nd, 2015.[18]
The tests were successful, with results exceeding expectations. Different fuel additives (such as TEOS) as well as different jet vane materials were also tested. The 2015 test firings used passive pressure blow-down.[18]
No more development or use for BPM-2 or -5 engines is planned. CS has primarily moved on to the use of the BPM-25 ahead of the planned development of the Spica rocket.[12]
Engines and propellant 2008–2014
[edit]From 2008 to 2012, the group based the work on a hybrid rocket, using liquid oxygen (LOX) as oxidizer.[19] Originally, the HEAT-1X rocket was to be fueled by paraffin wax, but a ground test 28 February 2010 revealed that some of the paraffin wax had only partially melted, instead of evaporating. The result was that HEAT-1X had less power than expected. A ground test firing of HEAT-1X-P (P for polyurethane) was conducted 16 May 2010. The polyurethane had the impulse required, but showed heavy oscillation.[20] Until 2011 the group had performed more than 30 tests of various engine types at their rocket engine test facility at Refshaleøen.[21] In fall of 2012 a concept engine using white fuming nitric acid and furfuryl alcohol was tried using a static test setup.[22] In 2012 a decision was made to switch to bi-propellant, liquid-fueled engines running on liquid oxygen and ethanol. This evolved into the BPM(Bi-Propellant Motor) class currently in use at CS as of 2024.[23]
HATV
[edit]The HATV (Hybrid Atmospheric Test Vehicle) was a planned sounding rocket. The HATV booster was successfully static fired, though it was never launched.[24]
HEAT-1X
[edit]HEAT 1X (Hybrid Exo Atmospheric Transporter)[25] was the rocket booster module intended to launch the space capsule Tycho Brahe into space, the combination being known as HEAT-1X TYCHO BRAHE. The rocket design was the result of numerous static-booster tests of the solid fuel epoxy and the liquid oxidizer nitrous oxide. A combination which was also used in the scale-down test rocket HATV (Hybrid Atmospheric Test Vehicle) which was only one third the size of the HEAT. Stabilization of the rocket was provided through rollerons. The rocket was launched on June 3rd, 2011. from the floating Sputnik platform.[26]
Within the first few seconds the rocket unexpectedly began to pitch over to approximately 30 degrees to horizontal. Due to the undesirable angle, the motor was manually commanded to shut down 16 seconds into flight at an altitude of 1.4 kilometers, with the rocket eventually rising to an apogee of approximately 2.8 kilometers, significantly off from the 30km goal.[27] The rocket landed 8.5 kilometers[28] away from the position where it was launched. The Tycho Brahe successfully separated from the booster, however, both the parachutes for the booster and Tycho Brahe did not successfully deploy. In the case of the Tycho Brahe, it was successfully recovered from the ocean after suffering a 26G impact upon landing.[27] It was found waterlogged and partially damaged. The booster sank to a depth of 80-90 meters.
TM-65 and TM-65 IIA and TM-65 IIB
[edit]TM-65 and TM6-5 IIA/B were liquid propellant engines using 75% Ethanol and liquid oxygen (LOX) as oxidizer. These engines produced about 65 kN thrust.[29] First static tests were conducted in May 2012. One TM65 II engine was for HEAT-2X and one was for HEAT-1600 LE. The TM-65 engine passed the test undamaged, and was fired at up to 50% of its rated thrust. The group planned to repeat the test with higher thrust levels, until the TM-65 class in 2014 was abandoned in favour of the BPM-100 engine concept.[30]
HEAT-2X
[edit]The HEAT-2X was a rocket built for flight-testing the TM-65 engine. It was planned to carry a 1:3 scale, 80 kg space capsule mock-up called the TDS-80 into the stratosphere above the Kárman Line.[31]
The rocket was not flown as it suffered an engine fire during a static test in the summer of 2014.[31] The rocket nozzle imploded and a welding seam opened resulting in the expulsion of all the ethanol fuel (some 500 L) in just three seconds resulting in a large fire which damaged part of the rocket. The engine failure and subsequent fire was filmed[32] up close with a high-speed camera, which although burned on the outside, survived the inferno enough for the film to be recovered. The fire damaged the onboard TM-65 engine enough to be unrepairable, leading to both the engine and HEAT-2X as a whole being retired to the CS museum.[33] This was one of the major deciding factors in choosing to retire the TM-65 class.
RC-A1 Rocket and Recruits Initiative
[edit]The Recruits Initiative, launched in 2021, was designed to attract and educate talented young individuals in the fields of rocket science and technology. The initiative also aimed at enhancing Danish expertise within the space and defense industries by fostering the development of skilled professionals. This project contributes to the success of the Spica project and it also strengthens the competitiveness of Danish businesses in the growing global space industry.
The Recruit Rocket is a single-stage rocket designed and developed by the recruits team at Copenhagen Suborbitals. The rocket measures 5 meters in length from nose to engine, with a total weight, including fuel, of approximately 165 kg. Instead of a turbopump, it is powered by a dynamic pressure-regulating system (DPR). The BPM5 engine has been refined to the maximum during the rocket’s development, and through optimizing the design, it has achieved an impressive performance of 10 kN. The rocket’s top speed with a 5 kN motor is estimated to be 475 m/s, which is 1710 km/h. The project has provided a unique opportunity for the new members to gain hands-on experience, not only with the fundamental aspects of rocket design but also equipping them with the ability to tackle the various challenges that arise during rocket projects. As of 2024, the rocket is set for static testing in early 2025.[34]
Space Capsules
[edit]Tycho Brahe
[edit]The micro space craft (MSC), named Tycho Brahe after the Danish astronomer, has a steel pressure hull with room for one passenger.[35]
The passenger would be able to view the outside through a Perspex dome.[25] The occupant would fly in a half-standing, half-sitting position in a specially designed seat and would be wearing anti-G trousers to avoid blackout. Another compartment contains both the high-speed drogue parachute and the low-speed main parachutes for deceleration. The volume of the MSC will provide the buoyancy in the water upon touchdown.[36]
The first MSC was christened "Tycho Brahe 1" and its first flight was not crewed, instead using a crash test dummy.[37] A new aluminum MSC called MAX-1 named after Maxime Faget was under development but has been abandoned, according to the group, due to the physiological problems associated with rapid acceleration of a human in standing position.[38] The craft is now on display in the Tycho Brahe Planetarium in Copenhagen.[39]
Tycho Deep Space
[edit]Tycho Deep Space is a space capsule developed by Kristian von Bengtson.[40] The first version officially named "Beautiful Betty" by Mikael Bertelsen, the capsule's protector.[41] The uncrewed capsule was launched on 12 August 2012 at sea by a test Launch Escape System, off the coast of Bornholm. The launch did not provide enough height for the parachute to deploy and the capsule was partly damaged on impact with the sea.[40] Due to this damage, the TDS was retired. The capsule is 2 m in diameter, allowing for an astronaut to be in a horizontal position relative to the acceleration during launch and landing. This is in opposition to the first-generation Tycho Brahe design that required the astronaut to stand inside.
Missions
[edit]The group originally focused on launching from a land based spaceport like Andøya, Kiruna, or Iceland[42] The focus then turned towards a sea launch just outside the territorial waters of Denmark. A permission to launch was given by Danish authorities, but the North Sea, a possibility suggested by Danish Civil Aviation Administration (Statens Luftfartsvæsen) was rejected in 2009 by the Danish Maritime Authority (Søfartsstyrelsen). They preferred another area, giving formal and written permission to launch from the military firing range ESD138/ESD139,[43] located at 55°02′57″N 15°36′11″E / 55.04917°N 15.60306°E in the Baltic Sea.[citation needed] It is just outside Nexø on the Danish island of Bornholm. Copenhagen Suborbitals then had to build a floating mobile launcher platform (MLP) called Sputnik, named after the first artificial satellite to be put into orbit. Their launch campaigns includes the following ships:[citation needed]
- MLP-Sputnik - At first had to be towed via submarine,[44] but later it had two diesel engines installed,[45] and now sails under its own power.
- MHV Hjortø - A Naval Home Guard vessel which serves as mission control and recovery vessel.[36]
2010: The first launch attempt
[edit]The first full-scale test-launch aimed at 30 km altitude was planned to be conducted off the coast of Bornholm between 30 August and 13 September 2010.[46] The vehicle carried a crash test dummy "Rescue Randy"[47] instead of a human pilot, with crewed flight not planned for some years. The success criteria were the completion of the sea voyage and a countdown with launch, with recovery planned as a bonus.[48]
On Tuesday, 31 August 2010, the privately built Danish submarine UC3 Nautilus pushed the launch platform Sputnik carrying the rocket and spacecraft from Copenhagen towards the launch area near Nexø, Bornholm.[49]
A launch attempt was made on Sunday, 5 September 2010, 14:43 CEST,[50] but the motor could not be started due to a failure of the LOX valve which is assumed to be caused by insufficient heating of the valve. The design famously included a consumer hair dryer[51] for defrosting the LOX-valve; in effect it was not the blow-dryer but its power supply that failed.[52]
The group promised to come back the year after to attempt the launch again.[53]
2011: First flight of HEAT-1X Tycho Brahe
[edit]Having done updates on the rocket, and the valve, and with MLP-Sputnik under her own power, and a support vessel, the group sailed again for Spaceport Nexø on May 28 at 4:50 a.m. They again met up with MHV Hjortø, a Naval Home Guard vessel that serves as mission control and recovery vessel. The second launch attempt was more successful and the maiden flight took place 3 June 2011,[19] at 16:32 local time (CEST) (14:32 GMT). The HEAT-1X rocket lifted off, but was only able to ascend to an altitude of only 2.8 km.[54] Mission Control had to shut the engine off early after 21 seconds.[55]
2012 Missions
[edit]SMARAGD Flight
[edit]The SMARAGD rocket (emerald in Danish) is a 5.7 meter[56] two-stage rocket weighing 160 kg, intended to reach an altitude in excess of 20km,[57] that was used for testing various technological aspects of the operation. On July 27, 2012, the team set out from Nexø towards the launch site, intending to launch the SMARAGD rocket.[58][59] After some initial problems with the remote launch control,[60] the rocket launched successfully just after 1 pm[61][62] and reached a maximum altitude of 8.2 km.[63] It was evident shortly after takeoff that the nosecone containing electronics broke off during launch, possibly due to the large acceleration of estimated 20 g.[64]
Tycho Deep Space / LES flight
[edit]On 12 August 2012 at 09:18, the space capsule Tycho Deep Space was launched to test a launch escape system. However the parachute did not deploy properly and the capsule was damaged on impact.[65] Several media had misunderstood the schedule and proclaimed the launch to have been started prematurely due to an error.[66] The test was considered partly successful by the team, due to the successful rocket launch and the unsuccessful parachute deployment.[67] The launch could be followed live via live streaming from several video cameras; additionally high-speed cameras were mounted on the MLP.[68]
2013 Missions
[edit]SAPPHIRE-1 Mission
[edit]SAPPHIRE-1, a modification of the HATV, was a 4.5 m rocket whose main purpose was to test the active guidance system developed by Copenhagen Suborbitals.[69] It was successfully launched on 23 June 2013.[70]
2016 Missions
[edit]Nexø I
[edit]Nexø I was launched Saturday, 23 July 2016, with inaugural BPM-5 engine. It was a partial success, and the supply of liquid oxygen to the engine was insufficient due to partial premature evaporation.[71][72]
2018 Missions
[edit]Nexø II
[edit]The Nexø II was successfully launched on 4 August 2018, with a slightly modified BPM-5 engine. It reached an apogee of 8–12 km and was safely recovered via parachute.[73]
Goals and records achieved
[edit]Copenhagen Suborbitals' achievements include:
- Most powerful amateur rocket ever flown.[74]
- First amateur rocket flown with a payload of a full-size crash test dummy.[75]
- First Main Engine(s) Cut-Off (MECO) command sent to, received and performed by an amateur rocket.[76]
- Handling and orchestration of a sea launch by a small-budget organization.[77]
On 3 October 2013, Copenhagen Suborbitals was awarded the "Breitling Milestone Trophy" award by Fédération Aéronautique Internationale at a ceremony in Kuala Lumpur.[78][79]
Support group
[edit]In 2010, an independent group of space enthusiasts founded the Copenhagen Suborbitals Support group (CSS).[80] The main purpose of this group is to "support CS economically, morally and practically in their mission". Within two days after its founding, CSS reached 100 members. November 15, 2011 marked a major milestone for CSS as 500 members was reached. As of early 2024, around 600 members were recorded.[80]
By paying a fixed monthly amount, the members of Copenhagen Suborbitals Support now cover most of the fixed costs for the project in addition to donating various forms of hardware.[81] By 2015, CS was supported with £12,500 per month.[82]
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External links
[edit]External media | |
---|---|
Images | |
Picasa Web album (many Wikipedia compatible licences) | |
Video | |
HEAT1X-Tycho launch highlights on YouTube | |
Lecture by Kristian von Bengtson on TEDx | |
Today Show video |
- Copenhagen Suborbitals official website
- Wired blog written by Kristian von Bengtson of Copenhagen Suborbitals
- Project overview on Ingeniøren
- Danish blog written by the people of Copenhagen Suborbitals