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MDA contracted with SpaceX to put the CASSIOPE payload on the first flight of an essentially new launch vehicle —a non-operational demonstration launch.<ref name=sfn20130928 /> The Falcon 9 v1.1, upgraded from the original Falcon 9, is a 60 percent heavier rocket with 60% more thrust.<ref name=sfn20130928>{{cite news |url=http://www.spaceflightnow.com/falcon9/006/130928preview/ |title=SpaceX to put Falcon 9 upgrades to the test Sunday |work=Spaceflight Now |first=Stephen |last=Clark |date=September 28, 2013 |accessdate=September 28, 2013}}</ref> The flight was contracted with a payload mass that is very small relative to the rocket's capability, at a discounted rate because it was a technology demonstration mission for SpaceX, approximately 20% of the normal published price for SpaceX Falcon 9 [[low Earth orbit|LEO]] missions.<ref name=sfn20130906>{{cite news |url=http://www.spacenews.com/article/launch-report/37094musk-says-spacex-being-%E2%80%9Cextremely-paranoid%E2%80%9D-as-it-readies-for-falcon-9%E2%80%99s |title=Musk Says SpaceX Being "Extremely Paranoid" as It Readies for Falcon 9's California Debut |work=Space News |first=Irene |last=Klotz |date=September 6, 2013 |accessdate=September 13, 2013}}</ref>
MDA contracted with SpaceX to put the CASSIOPE payload on the first flight of an essentially new launch vehicle —a non-operational demonstration launch.<ref name=sfn20130928 /> The Falcon 9 v1.1, upgraded from the original Falcon 9, is a 60 percent heavier rocket with 60% more thrust.<ref name=sfn20130928>{{cite news |url=http://www.spaceflightnow.com/falcon9/006/130928preview/ |title=SpaceX to put Falcon 9 upgrades to the test Sunday |work=Spaceflight Now |first=Stephen |last=Clark |date=September 28, 2013 |accessdate=September 28, 2013}}</ref> The flight was contracted with a payload mass that is very small relative to the rocket's capability, at a discounted rate because it was a technology demonstration mission for SpaceX, approximately 20% of the normal published price for SpaceX Falcon 9 [[low Earth orbit|LEO]] missions.<ref name=sfn20130906>{{cite news |url=http://www.spacenews.com/article/launch-report/37094musk-says-spacex-being-%E2%80%9Cextremely-paranoid%E2%80%9D-as-it-readies-for-falcon-9%E2%80%99s |title=Musk Says SpaceX Being "Extremely Paranoid" as It Readies for Falcon 9's California Debut |work=Space News |first=Irene |last=Klotz |date=September 6, 2013 |accessdate=September 13, 2013}}</ref>

Since this was the [[Falcon 9 Flight 6|first flight of a new launch vehicle]], the US Air Force had estimated the overall probability of failure on the mission was nearly fifty percent.<ref name=faa20130823>
{{cite news |url=https://www.federalregister.gov/articles/2013/08/27/2013-20726/waiver-to-space-exploration-technologies-corporation-of-acceptable-risk-limit-for-launch |title=Waiver to Space Exploration Technologies Corporation of Acceptable Risk Limit for Launch: A Notice by the Federal Aviation Administration on 08/27/2013 |work=Federal Register |publisher=United States Government |date=2013-08-23 |accessdate=2016-01-21 |quote=The Falcon 9 v1.1 is a new launch vehicle. The U.S. Air Force has determined that its overall failure probability is nearly fifty percent for each of the first two launches. }}</ref> In the event, the mission was successful, as was each of the next 13 Falcon 9 v1.1 missions before a launch vehicle failure and loss of mission occurred on [[Falcon 9 Flight 19]] in June 2015.


The Falcon 9 upper stage used to launch CASSIOPE was left [[:Category:Derelict satellites orbiting Earth|derelict]] in a decaying [[elliptic orbit|elliptical]] low Earth orbit that, nearly one year later ({{asof|2014|09|13|lc=y}}), had a [[perigee]] of {{convert|328|km|mi|abbr=on|sp=us}} and an [[apogee]] of {{convert|1408|km|mi|abbr=on|sp=us}}.<ref name=n2yo-F9f11ss>
The Falcon 9 upper stage used to launch CASSIOPE was left [[:Category:Derelict satellites orbiting Earth|derelict]] in a decaying [[elliptic orbit|elliptical]] low Earth orbit that, nearly one year later ({{asof|2014|09|13|lc=y}}), had a [[perigee]] of {{convert|328|km|mi|abbr=on|sp=us}} and an [[apogee]] of {{convert|1408|km|mi|abbr=on|sp=us}}.<ref name=n2yo-F9f11ss>

Revision as of 07:35, 21 January 2016

CASSIOPE
Mission typeTechnology
Communications
Research
OperatorMDA
COSPAR ID2013-055A Edit this at Wikidata
SATCAT no.39265
Websitehttp://www.asc-csa.gc.ca/eng/satellites/cassiope.asp
Mission durationPrimary mission: 18 months[1]
Design life: 2 years[2][3]
Elapsed: 11 years, 1 month and 30 days
Orbits completed6763[4]
Spacecraft properties
BusMAC-200
ManufacturerMDA (prime)
Magellan Aerospace (subcontractor)
Com Dev (subcontractor)
Launch mass500 kg (1,100 lb)[3]
Dimensions180×125 cm (71×49 in)[3]
Power5 solar panels generating
up to 600 W[3]
Start of mission
Launch dateSeptember 29, 2013, 16:00 (2013-09-29UTC16Z) UTC
RocketFalcon 9 v1.1
Launch siteVandenberg SLC-4E
ContractorSpaceX
Orbital parameters
Reference systemGeocentric
RegimeLow Earth
Semi-major axis7,240.49 km (4,499.03 mi)[4]
Eccentricity0.0744616[4]
Perigee altitude330 km (210 mi)[4]
Apogee altitude1,408 km (875 mi)[4]
Inclination80.98 degrees[4]
Period102.19 minutes[4]
RAAN192.36 degrees[4]
Argument of perigee243.84 degrees[4]
Mean anomaly14.09 degrees[4]
Mean motion14.09[4]
EpochJanuary 24, 2015, 21:55:19 UTC[4]

CASSIOPE, or CAScade, Smallsat and IOnospheric Polar Explorer,[5] is a Canadian Space Agency (CSA) multi-mission satellite operated by MacDonald, Dettwiler and Associates (MDA). The mission is funded through CSA and the Technology Partnerships Canada program.[5] It was launched September 29, 2013, on the first flight of the SpaceX Falcon 9 v1.1 launch vehicle.[2][6] CASSIOPE is the first Canadian hybrid satellite to carry a dual mission in the fields of telecommunications and scientific research. The main objectives are to gather information to better understand the science of space weather, while verifying high-speed communications concepts through the use of advanced space technologies.

The satellite was deployed in an elliptical[7] polar orbit[8] and carries a commercial communications system called Cascade as well as a scientific experiment package called e-POP (enhanced Polar Outflow Probe).[8]

Following separation of the Falcon 9's first stage, it was used by SpaceX for a controlled descent and landing test. While the first stage was destroyed on impact with the ocean, significant data was acquired and the test was considered a success.[9]

Spacecraft

CASSIOPE is a 500 kg (1,100 lb) small satellite that is 180 cm (5.9 ft) long and 125 cm (4.10 ft) high. It combines the function of two distinct missions in order to be more cost-effective and reduce risk.[10]

The spacecraft carries a primary payload of two instrument suites: the Cascade commercial communications system and a scientific payload named e-POP.

Cascade

The commercial payload, named Cascade, is a technology demonstrator courier in the sky, aimed a providing a proof of concept for a digital broadband courier service for commercial use. Built by MDA, the operational concept is to receive very large data files as the satellite orbits the globe, store them onboard temporarily, then deliver them at a later time to nearly any destination worldwide.[10]

The demonstrator will provide a secure digital store-and-forward file delivery service, exploiting the fact that CASSIOPE passes over much of the globe 15 times per day. It has been described[by whom?] as a courier service, with the customers using a small parabolic antenna of one or two meters (three or six feet) to upload or download files at a rate of 1.2 gigabits per second. The storage capacity will be between 50 and 500 gigabytes and the data delivery time will be about 90 minutes, depending on the pickup and deposit points on the globe.[citation needed]

e-POP

The e-POP portion of CASSIOPE is a suite of eight scientific instruments. The University of Calgary's Institute for Space Research leads the science project, while MDA is the prime contractor for the mission including launch and operation of the spacecraft. The orbital science mission is scheduled for a 21-month duration.[8]

e-POP will gather data on Solar storms in the upper atmosphere. These storms give rise to the polar aurora or northern lights seen in the skies in northern latitudes. While these atmospheric glows may offer a thrilling night time spectacle, the inducing radiation can interfere with radio communications, GPS navigation, and other space-based systems.[citation needed] The eight scientific instruments aboard CASSIOPE will help scientists understand solar weather and eventually plan for measures to mitigate its deleterious effects.[7]

The e-POP payload contains eight scientific instruments:[11]

  • Coherent EM Radio Tomography (CER), measuring radio propagation and ionospheric scintillation
  • Fast Auroral Imager (FAI), measuring large-scale auroral emissions
  • GPS Altitude and Profiling Experiment (GAP), high-precision position and attitude determination
  • Imaging and Rapid Scanning Ion Mass Spectrometer (IRM), measuring the three-dimensional distribution of ions
  • Fluxgate Magnetometer (MGF), high-precision magnetic field perturbation measurement
  • Neutral Mass Spectrometer (NMS), measuring the mass, composition and velocity of neutral particles
  • Radio Receiver Instrument (RRI), measuring radio wave propagation
  • Suprathermal Electron Imager (SEI), measuring low-energy electron distribution

History

The satellite that became CASSIOPE began with a 1996 concept for a small (70 kg/150 lb), inexpensive microsatellite called Polar Outflow Probe, or POP. The Canadian Space Agency funded a 1997 feasibility study that led to a modified mission concept that was designed during 2000-2005.[8] The revised concept was to combine an enhanced version of POP, called e-POP, with an MDA Corporation commercial satellite called Cascade, into a single satellite, and to design and build a generic, low-cost small satellite bus that would be useful for other Canadian satellite missions in the future.

The eight e-POP scientific instruments were built, calibrated, and tested in 2005-2007, with integration onto the satellite bus for spacecraft-level testing in 2008-2009.[8]

Launch

The satellite was launched on September 29, 2013 aboard a SpaceX Falcon 9 v1.1 rocket.[12]

SpaceX Falcon 9 launch from Vandenberg with CASSIOPE

At the time the launch was contracted in 2005, a SpaceX Falcon 1 was the planned launch vehicle. The launch was originally scheduled for 2008 from Omelek Island. The launch date slipped several times, and after SpaceX discontinued the Falcon 1, the launch was shifted to the much larger Falcon 9 in June 2010.[7][13]

MDA contracted with SpaceX to put the CASSIOPE payload on the first flight of an essentially new launch vehicle —a non-operational demonstration launch.[14] The Falcon 9 v1.1, upgraded from the original Falcon 9, is a 60 percent heavier rocket with 60% more thrust.[14] The flight was contracted with a payload mass that is very small relative to the rocket's capability, at a discounted rate because it was a technology demonstration mission for SpaceX, approximately 20% of the normal published price for SpaceX Falcon 9 LEO missions.[15]

Since this was the first flight of a new launch vehicle, the US Air Force had estimated the overall probability of failure on the mission was nearly fifty percent.[16] In the event, the mission was successful, as was each of the next 13 Falcon 9 v1.1 missions before a launch vehicle failure and loss of mission occurred on Falcon 9 Flight 19 in June 2015.

The Falcon 9 upper stage used to launch CASSIOPE was left derelict in a decaying elliptical low Earth orbit that, nearly one year later (as of 13 September 2014), had a perigee of 328 km (204 mi) and an apogee of 1,408 km (875 mi).[17]

Post-mission launch vehicle testing

Main article: Falcon 9 booster landing tests

After the second stage separated from the booster stage, SpaceX conducted a novel flight test where the booster conducted a test to attempt to reenter the lower atmosphere in a controlled manner and decelerate to a simulated over-water landing.[18] The test was successful, but the booster stage was not recovered.

After the three-minute boost phase of September 29, 2013 launch, the booster stage attitude was reversed, and three of the nine engines refired at high altitude, as planned, to initiate the deceleration and controlled descent trajectory to the surface of the ocean. The first phase of the test worked well and the first stage re-entered safely.[12]

However, the first stage began to roll due to aerodynamic forces during the descent through the atmosphere, and the roll rate exceeded the capabilities of the booster attitude control system (ACS) to null it out. The fuel in the tanks centrifuged to the outside of the tank and the single engine involved in the low-altitude deceleration maneuver shut down. Debris from the first stage was subsequently retrieved from the ocean.[12]

SpaceX also ran a post-mission test on the second stage. While a number of the new capabilities were successfully tested on the September 29, 2013, CASSIOPE flight, there was an issue with the second stage restart test. The test to reignite the second stage Merlin 1D vacuum engine once the rocket had deployed its primary payload (CASSIOPE) and all of its nanosat secondary payloads was unsuccessful.[9] The engine failed to restart while the second stage was coasting in low Earth orbit.

Secondary payloads

Five nanosatellite spacecraft that were also carried to orbit on the same launch vehicle that carried the CASSIOPE primary payload:[10]

References

  1. ^ Howell, Elizabeth (September 27, 2013). "SpaceX to Launch Space Weather Satellite for Canada Sunday". Space.com. Retrieved April 13, 2014.
  2. ^ a b Graham, William (September 29, 2013). "SpaceX successfully launches debut Falcon 9 v1.1". NASA Spaceflight. Retrieved April 13, 2014.
  3. ^ a b c d "CASSIOPE/e-POP Fact Sheet". University of Calgary. 2014. Retrieved April 14, 2014.
  4. ^ a b c d e f g h i j k l "CASSIOPE Satellite details 2013-055A NORAD 39265". N2YO. January 24, 2015. Retrieved January 25, 2015.
  5. ^ a b Giffin, Gregory B.; Ressl, Waqar-Un-Nissa; Yau, Andrew W.; King, E. Peter (2004). Cassiope: A Canadian Smallsat-Based Space Science and Advanced Satcom Demonstration Mission. 18th AIAA/USU Conference on Small Satellites. Logan, Utah. August 9–12, 2004. SSC04-VI-5.
  6. ^ Foust, Jeff (March 27, 2013). "After Dragon, SpaceX's focus returns to Falcon". NewSpace Journal. Retrieved April 5, 2013.
  7. ^ a b c Boucher, Mark (June 26, 2012). "Canada's CASSIOPE Satellite Nearing Liftoff". SpaceRef Canada. Retrieved September 7, 2013.
  8. ^ a b c d e "e-POP Project Schedule". University of Calgary. 2013. Retrieved September 6, 2013.
  9. ^ a b Ferster, Warren (September 29, 2013). "Upgraded Falcon 9 Rocket Successfully Debuts from Vandenberg". Space News. Retrieved September 30, 2013.
  10. ^ a b c Messier, Doug (September 10, 2013). "A Preview of Falcon 9′s Flight From Vandenberg". Parabolic Arc. Retrieved September 11, 2013.
  11. ^ "e-POP Payload on CASSIOPE". University of Calgary. 2013. Retrieved February 20, 2014.
  12. ^ a b c Messier, Doug (September 29, 2013). "Falcon 9 Launches Payloads into Orbit From Vandenberg". Parabolic Arc. Retrieved September 30, 2013.
  13. ^ Boucher, Mark (June 28, 2010). "Old News Revisited - SpaceX to Launch CASSIOPE". SpaceRef Canada. Retrieved September 7, 2013.
  14. ^ a b Clark, Stephen (September 28, 2013). "SpaceX to put Falcon 9 upgrades to the test Sunday". Spaceflight Now. Retrieved September 28, 2013.
  15. ^ Klotz, Irene (September 6, 2013). "Musk Says SpaceX Being "Extremely Paranoid" as It Readies for Falcon 9's California Debut". Space News. Retrieved September 13, 2013.
  16. ^ "Waiver to Space Exploration Technologies Corporation of Acceptable Risk Limit for Launch: A Notice by the Federal Aviation Administration on 08/27/2013". Federal Register. United States Government. August 23, 2013. Retrieved January 21, 2016. The Falcon 9 v1.1 is a new launch vehicle. The U.S. Air Force has determined that its overall failure probability is nearly fifty percent for each of the first two launches.
  17. ^ "FALCON 9 R/B details 2013-055G NORAD 39271". N2YO. Retrieved September 13, 2014.
  18. ^ Lindsey, Clark (March 28, 2013). "SpaceX moving quickly towards fly-back first stage". NewSpace Watch. Archived from the original on April 16, 2013. Retrieved March 29, 2013.
  19. ^ Holemans, Walter; Moore, R. Gilbert; Kang, Jin (2012). Counting Down to the Launch of POPACS (Polar Orbiting Passive Atmospheric Calibration Spheres). 26th Annual AIAA/USU Conference on Small Satellites. August 13–16, 2012. Utah State University. SSC12-X-3.

Further reading

  • CASSIOPE at the Canadian Space Agency
  • CASSIOPE at MacDonald, Dettwiler and Associates
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