OICETS: Difference between revisions
Tom.Reding (talk | contribs) m →top: WL 2 first-publishers; WP:GenFixes on; using AWB |
m Grammar |
||
(18 intermediate revisions by 14 users not shown) | |||
Line 3: | Line 3: | ||
| name = Optical Inter-orbit Communications Engineering Test Satellite |
| name = Optical Inter-orbit Communications Engineering Test Satellite |
||
| names_list = OICETS, ''Kirari'' |
| names_list = OICETS, ''Kirari'' |
||
| image = |
| image = File:JAXA Kiriani test satelite.jpg |
||
| image_caption = |
| image_caption = |
||
| image_size = |
| image_size =150px |
||
| mission_type = Technology demonstration |
| mission_type = Technology demonstration |
||
| operator = [[JAXA]] |
| operator = [[JAXA]] |
||
| COSPAR_ID = |
| COSPAR_ID = 2005-031A |
||
| SATCAT = 28809 |
| SATCAT = 28809 |
||
| website = {{URL|http://global.jaxa.jp/projects/sat/oicets/index.html}} |
| website = {{URL|http://global.jaxa.jp/projects/sat/oicets/index.html}} |
||
Line 20: | Line 20: | ||
| power = <!--end-of-life power, in watts--> |
| power = <!--end-of-life power, in watts--> |
||
| launch_date = {{start-date|23 August 2005, 21:10}} UTC<ref name="nssdc-orbit">{{cite web |url= |
| launch_date = {{start-date|23 August 2005, 21:10}} UTC<ref name="nssdc-orbit">{{cite web |url=https://nssdc.gsfc.nasa.gov/nmc/spacecraft/display.action?id=2005-031A |title=OICETS - Trajectory Details |work=[[National Space Science Data Center]] |publisher=[[NASA]] |access-date=7 January 2017}}</ref> |
||
| launch_rocket = [[Dnepr (rocket)|Dnepr]]<ref name="astronautix">{{cite |
| launch_rocket = [[Dnepr (rocket)|Dnepr]]<ref name="astronautix">{{cite encyclopedia |url=http://www.astronautix.com/k/kirari.html |archive-url=https://web.archive.org/web/20161221095254/http://www.astronautix.com/k/kirari.html |url-status=dead |archive-date=21 December 2016 |title=Kirari |encyclopedia=Encyclopedia Astronautica |access-date=7 January 2017}}</ref> |
||
| launch_site = [[Baikonur Cosmodrome|Baikonur]] [[Baikonur Cosmodrome Site 109|Pad 109/95]]<ref name="astronautix" /> |
| launch_site = [[Baikonur Cosmodrome|Baikonur]] [[Baikonur Cosmodrome Site 109|Pad 109/95]]<ref name="astronautix" /> |
||
| launch_contractor = <!--United Launch Alliance, Arianespace, etc--> |
| launch_contractor = [[ISC Kosmotras]]<!--United Launch Alliance, Arianespace, etc--> |
||
| entered_service = <!--date on which the spacecraft entered service, if it did not do so immediately after launch--> |
| entered_service = <!--date on which the spacecraft entered service, if it did not do so immediately after launch--> |
||
| disposal_type = Decommissioned |
| disposal_type = Decommissioned |
||
| deactivated = {{end-date|24 September 2009, 05:48}} UTC<ref name="jaxa20090924">{{cite web |url=http://global.jaxa.jp/projects/sat/oicets/topics.html |title=Kirari: Signals stopped; successful operation ends |publisher=[[JAXA]] |date=24 September 2009 | |
| deactivated = {{end-date|24 September 2009, 05:48}} UTC<ref name="jaxa20090924">{{cite web |url=http://global.jaxa.jp/projects/sat/oicets/topics.html |title=Kirari: Signals stopped; successful operation ends |publisher=[[JAXA]] |date=24 September 2009 |access-date=7 January 2017}}</ref> |
||
| decay_date = <!--when craft re-entered the atmosphere, not needed if it landed--> |
| decay_date = <!--when craft re-entered the atmosphere, not needed if it landed--> |
||
Line 47: | Line 47: | ||
}} |
}} |
||
The '''Optical Inter-orbit Communications Engineering Test Satellite''' ('''OICETS'''), also called '''''Kirari''''', |
The '''Optical Inter-orbit Communications Engineering Test Satellite''' ('''OICETS'''), also called '''''Kirari''''', was an experimental satellite launched by [[JAXA]] to demonstrate interorbital communication between satellites through optical (laser) means. OICETS was originally slated for a launch on the second [[J-I]] launcher. Due to problems with that launcher, the launch had to be put on hold. Using the [[H-IIA]] was out of question: it would have been overkill to use the H-IIA to send a {{convert|570|kg|lb}} satellite into [[low Earth orbit]], and there was no budget for another H-IIA launch. Finally, in order to be able to perform the tests during the lifetime of the European [[Artemis (satellite)|Artemis]] satellite (since 2014, sold to [[Avanti Communications]] to exploit its Ka, S, and L-band payloads), OICETS was successfully launched on a Russian-Ukrainian [[Dnepr rocket]]. |
||
The satellite was decommissioned and its mission terminated on 24 September 2009 at 05:48 UTC.<ref name="jaxa20090924" /> |
The satellite was decommissioned and its mission terminated on 24 September 2009 at 05:48 UTC.<ref name="jaxa20090924" /> |
||
Line 69: | Line 69: | ||
[[Category:Spacecraft launched in 2005]] |
[[Category:Spacecraft launched in 2005]] |
||
[[Category:Spacecraft launched by Dnepr rockets]] |
[[Category:Spacecraft launched by Dnepr rockets]] |
||
[[Category:Spacecraft decommissioned in 2009]] |
|||
[[Category:Technology demonstration satellites]] |
|||
{{Japan-spacecraft-stub}} |
{{Japan-spacecraft-stub}} |
Latest revision as of 10:42, 13 November 2024
Names | OICETS, Kirari | ||||||
---|---|---|---|---|---|---|---|
Mission type | Technology demonstration | ||||||
Operator | JAXA | ||||||
COSPAR ID | 2005-031A | ||||||
SATCAT no. | 28809 | ||||||
Website | global | ||||||
Mission duration | Planned: 1 year Final: 4 years, 1 month | ||||||
Spacecraft properties | |||||||
Manufacturer | Toshiba | ||||||
Launch mass | 570 kg (1,260 lb) | ||||||
Dimensions | 0.78 × 1.1 × 1.5 m (2.6 × 3.6 × 4.9 ft) | ||||||
Start of mission | |||||||
Launch date | 23 August 2005, 21:10[1] | UTC||||||
Rocket | Dnepr[2] | ||||||
Launch site | Baikonur Pad 109/95[2] | ||||||
Contractor | ISC Kosmotras | ||||||
End of mission | |||||||
Disposal | Decommissioned | ||||||
Deactivated | 24 September 2009, 05:48[3] | UTC||||||
Orbital parameters | |||||||
Reference system | Geocentric | ||||||
Regime | Low Earth | ||||||
Eccentricity | 0.00107 | ||||||
Perigee altitude | 597 km (371 mi) | ||||||
Apogee altitude | 612 km (380 mi) | ||||||
Inclination | 97.8° | ||||||
Period | 96.8 minutes | ||||||
Epoch | 23 August 2005, 17:10:00 UTC[1] | ||||||
| |||||||
The Optical Inter-orbit Communications Engineering Test Satellite (OICETS), also called Kirari, was an experimental satellite launched by JAXA to demonstrate interorbital communication between satellites through optical (laser) means. OICETS was originally slated for a launch on the second J-I launcher. Due to problems with that launcher, the launch had to be put on hold. Using the H-IIA was out of question: it would have been overkill to use the H-IIA to send a 570 kilograms (1,260 lb) satellite into low Earth orbit, and there was no budget for another H-IIA launch. Finally, in order to be able to perform the tests during the lifetime of the European Artemis satellite (since 2014, sold to Avanti Communications to exploit its Ka, S, and L-band payloads), OICETS was successfully launched on a Russian-Ukrainian Dnepr rocket.
The satellite was decommissioned and its mission terminated on 24 September 2009 at 05:48 UTC.[3]
Achievements
[edit]- On 9 December 2005, JAXA succeeded in establishing optical links between OICETS and Artemis.
- During March 2006, a successful link between OICETS and a ground station in Japan was established. This was the first optical links connection between a fixed ground station and an LEO satellite.
- On 7 June 2006, JAXA established a communication link between OICETS and a mobile ground station operated by the German Aerospace Center (DLR).
Notes
[edit]- ^ a b "OICETS - Trajectory Details". National Space Science Data Center. NASA. Retrieved 7 January 2017.
- ^ a b "Kirari". Encyclopedia Astronautica. Archived from the original on 21 December 2016. Retrieved 7 January 2017.
- ^ a b "Kirari: Signals stopped; successful operation ends". JAXA. 24 September 2009. Retrieved 7 January 2017.
External links
[edit]- OICETS website at JAXA.jp