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This page is an alphabetic list of ]es, of which multiple similar ]s have been, or are being, built to the same ] of structural frame, propulsion, spacecraft power and intra-spacecraft communication. | This page is an alphabetic list of ]es, of which multiple similar ]s have been, or are being, built to the same ] of structural frame, propulsion, spacecraft power and intra-spacecraft communication. | ||
==Satellite buses== | Fas of==Satellite buses== | ||
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| 25<ref name=os2012/><small>(as of early 2012</small> | | 25<ref name=os2012/><small>(as of early 2012)</small> | ||
| Operational | | Operational | ||
| 1997<ref name=os2012>{{cite web |url=http://www.orbital.com/NewsInfo/Publications/GEO_Brochure.pdf |title=GEOStar Brochure |date=2012 |publisher=Orbital Sciences |accessdate=2013-09-20 }}</ref> | | 1997<ref name=os2012>{{cite web |url=http://www.orbital.com/NewsInfo/Publications/GEO_Brochure.pdf |title=GEOStar Brochure |date=2012 |publisher=Orbital Sciences |accessdate=2013-09-20 }}</ref> |
Revision as of 20:03, 20 September 2013
This page is an alphabetic list of satellite buses, of which multiple similar artificial satellites have been, or are being, built to the same model of structural frame, propulsion, spacecraft power and intra-spacecraft communication.
Fas of==Satellite buses==
Satellite bus | Origin | Manufacturer | Maximum Satellite Payload Mass (kg) |
Total Mass (fueled bus plus sat payload) (kg) |
Price (Mil US$) |
Launches | Status | First flight | Last flight | Comment |
---|---|---|---|---|---|---|---|---|---|---|
A2100 | United States | Lockheed Martin | 37 as of 2011 | Operational | 1996 | 2013 | GEO | |||
Arkyd 100 | United States | Planetary Resources | 11–15 kg | Development | Arkyd 100 | |||||
ATK 100 | United States | ATK Space Systems and Services | 15 kg | Operational | ATK 100 | |||||
ATK 200 | United States | ATK Space Systems and Services | 200 kg | Operational | Formerly named, "Responsive Space Modular Bus"; used on ORS-1 and EO-1 | |||||
ATK 500 | United States | ATK Space Systems and Services | 500 kg | 0 | Development | 2015 | MEO/GEO/HEO/GSO; formerly named, "High End Modular Bus"; planned for DARPA Phoenix | |||
ATK 700 | United States | ATK Space Systems and Services | 1,700 kg | 0 | Development | 2014? | GEO/LEO/MEO/HEO/GTO; ViviSat | |||
CubeSat Kit | United States | Pumpkin Inc. | 1 kg | 0 | Development | LEO; | ||||
Eurostar | France, Great Britain, | EADS Astrium | 6,400 kg | 40+ | Operational | 1990 | GEO | |||
HS-333 | United States | Hughes Space and Communications | 54 kg | 560 kg | 8 | Retired | 1972 | 1979 | GEO; first satellite series; eight built, 300 watt, 12-channel, single-antenna | |
I-1K | India | Antrix Corporation | 1,300+ kg | Operational | I-1000, Ideal for most small communication and meteorological satellites | |||||
I-2K | India | Antrix Corporation | 1,540 kg - 2,800 kg | Operational | I-2000,ideal for most of medium level communication payloads | |||||
I-3K | India | Antrix Corporation | 3,000+ kg | Operational | I-3000, Advanced communication satellites of 3000 kg class with DC power up to 4.5k | |||||
I-4K | India | Antrix Corporation | 5,000 kg (approx.) | Development | I-4000 | |||||
LS-1300 | United States | Space Systems/Loral | 5,500–6700 kg | 30 | Operational | 1984 | 2012 | GEO; previously named the FS-1300 | ||
Modular Common Spacecraft Bus | United States | NASA Ames Research Center | 383+ kg | 1 | Operational | 2013 LADEE | Very low-cost bus, capable of Lunar, Asteroidal, and Earth orbit missions. | |||
RS-300 | United States | Ball Aerospace | 125+ kg | 0 | Operational (as of 2009) |
RS-300 | ||||
SI-100 | Korea | Satrec | 100 kg | Development | SI-100 | |||||
SI-200 | Korea | Satrec | 200 kg | Operational | SI-200 | |||||
SI-300 | Korea | Satrec | 300 kg | ? | SI-300 | |||||
SNC-100 | United States | SNC Space Systems | 100 kg | 0 | Development | 2013 | SNC-100 | |||
SNC-100-L1 | United States | SNC Space Systems | 100 kg | 0 | Development | Optimized for LauncherOne | ||||
Spacebus 100 | France | Thales Alenia Space | 1,170 kg | 3 | Unknown | 1981 | 1981 | GEO | ||
Spacebus 300 | France | Thales Alenia Space | 2,100 kg (approx.) | 5 | Retired | 1987 | 1990 | GEO | ||
Spacebus 2000 | France | Thales Alenia Space | 1,900 kg (approx.) | 11 | Retired | 1990 | 1998 | GEO | ||
Spacebus 3000 | France | Thales Alenia Space | 2,800-3200 kg (approx.) | 27 | Operational | 1996 | 2010 | GEO | ||
Spacebus 4000 | France | Thales Alenia Space | 3,000-5700 kg (approx.) | 29 | Operational | 2005 | 2012 | GEO | ||
SpaceEye-1 | Korea | Satrec | 300 kg | ? | SpaceEye-1 | |||||
SpaceEye-2 | Korea | Satrec | 200 kg | ? | SpaceEye-2 | |||||
SpaceEye-10 | Korea | Satrec | 100 kg | ? | SpaceEye-10 | |||||
STAR-1 and STAR 2 | United States | Orbital Sciences | 25(as of early 2012) | Operational | 1997 | 2013 | GEO | |||
SSTL-100LO | United Kingdom | Surrey Satellite Technology | 100 kg | 0 | Development | Optimized for LauncherOne |
Legend for abbreviations in the table: Template:MultiCol
- GEO - Geostationary orbit
- GSO - Geosynchronous orbit
- GTO - Geostationary transfer orbit
| class="col-break " |
- HCO - Heliocentric orbit
- HEO - High Earth orbit
- LEO - Low Earth orbit
| class="col-break " |
- MEO - Medium Earth orbit
- SSO - Sun-synchronous orbit
- TLI - Trans Lunar Injection
See also
References
- "Lockheed Martin-Built A2100 Satellite Achieves 15 Year On-Orbit Life"
- Heater, Bryan (2013-01-21). "Planetary Resources shows off Arkyd-100 prototype, gives a tour of its workspace". Engadget. Retrieved 2013-01-23.
- Mike Wall (2013-04-24). "Private Asteroid-Mining Project Launching Tiny Satellites in 2014". Space.com. Retrieved 2013-04-25.
- Eric Anderson (30 Aug 2012). Eric Anderson – The Arkyd Series (video interview). moonandback.com. Retrieved 2012-09-06.
- ^
Werner, Debra (2012-08-13). "Builder Packing More Capability into Small Satellites". Space News. p. 13.
{{cite news}}
:|access-date=
requires|url=
(help) -
"ATK: Introducing the expanded product line of agile spacecraft buses". Space News. 2012-08-13. pp. 16–17.
ATK A100 THEMIS; ATK A200 ORS-1, TacSat3, and EO-1; ATK A500 DARPA Phoenix; ATK A700 ViviSat
- Hughes Aircraft Corporation, Space and Communications Group, SBS F6 Prime sales brochure, 1985
- ^ Krebs, Gunter. "Hughes: HS-333 / HS-356". Gunter's Space Page. Retrieved 4 July 2012.
- "SPACECRAFT SYSTEMS AND SUB SYSTEMS". Antrix Corporation. Retrieved 2013-02-02.
- "SPACECRAFT SYSTEMS AND SUB SYSTEMS". Antrix Corporation. Retrieved 2013-02-02.
- "SPACECRAFT SYSTEMS AND SUB SYSTEMS". Antrix Corporation. Retrieved 2013-02-02.
- ^ "Space Service Loral (SSL): LS-1300". Gunter's Space Page. Retrieved 2012-08-25. Cite error: The named reference "GSP20120825" was defined multiple times with different content (see the help page).
-
|
Graham, William (2013-09-06). . NASAspaceflight.com. Retrieved 2013-09-07.
{{cite news}}
: Check|url=
value (help) - NASA Lunar Science Institute, Common Spacecraft Bus for Lunar Explorer Missions, includes video.
- Krebs, Gunter. "Ball: RS-300". Gunter's Space Page. Retrieved 21 March 2011.
- Wade, Mark. "Satrec". Encyclopedia Astronautica. Retrieved 2012-09-16.
- Krebs, Gunter (2012-02-09). "Satrec Initiative: SI-200". Skyrocket.de (Gunter's Space Page). Retrieved 2012-09-16.
- ^ "Satellite System Products". Satrec Initiative. 2012. Retrieved 2012-09-16.
-
"SN-100 Small Satellite Production Line". Space News. 2012-08-13. p. 21.
first 18 satellites in production
- ^
"Virgin Galactic relaunches its smallsat launch business". NewSpace Journal. 2012-07-12. Retrieved 2012-08-25.
develop versions of their smallsat bus optimized to the design of LauncherOne."
Cite error: The named reference "nsj20120711" was defined multiple times with different content (see the help page). -
Harland, David M (2005). Space Systems Failures (2006 ed.). Chichester: Springer-Praxis. p. 221. ISBN 0-387-21519-0.
{{cite book}}
: Unknown parameter|coauthors=
ignored (|author=
suggested) (help) - ^ "GEOStar Brochure" (PDF). Orbital Sciences. 2012. Retrieved 2013-09-20.
Notes
It is not clear from the sources if the Spacebus 100 satellite bus is still on offer.
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