Comparison of satellite buses: Difference between revisions
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| [[Modular Common Spacecraft Bus]] |
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| Very low-cost bus, capable of [[Selenocentric orbit|Lunar]], [[heliocentric orbit|Asteroidal]], and [[Earth orbit]] missions.<ref>NASA Lunar Science Institute, [http://lunarscience.arc.nasa.gov/articles/common-spacecraft-bus-for-lunar-explorer-missions Common Spacecraft Bus for Lunar Explorer Missions], includes video.</ref> |
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| [[RS-300]] |
| [[RS-300]] |
Revision as of 17:23, 7 September 2013
This page is an alphabetic list of satellite bus designs representing multiple similar artificial satellites being built to the same basic design.
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 |
---|---|---|---|---|---|---|---|---|---|---|
Arkyd 100 | United States | Planetary Resources | Development[1] | Arkyd 100 | ||||||
ATK 100 | United States | ATK Space Systems and Services | 15 kg[2] | Operational | ATK 100 | |||||
ATK 200 | United States | ATK Space Systems and Services | 200 kg[2] | Operational | Formerly named, "Responsive Space Modular Bus"; used on ORS-1 and EO-1[2] | |||||
ATK 500 | United States | ATK Space Systems and Services | 500 kg[2] | 0 | Development | 2015 | MEO/GEO/HEO/GSO; formerly named, "High End Modular Bus"; planned for DARPA Phoenix[2] | |||
ATK 700 | United States | ATK Space Systems and Services | 1,700 kg[2] | 0 | Development | 2014? | GEO/LEO/MEO/HEO/GTO; ViviSat[3] | |||
CubeSat Kit[2] | 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[4] | 560[5] | 8[5] | Retired | 1972 | 1979[5] | GEO; first satellite series; eight built, 300 watt, 12-channel, single-antenna | |
LS-1300 | United States | Space Systems/Loral | 5,500–6700 kg[6] | > 30 | Operational | 1984[6] | 2012 | GEO; previously named the FS-1300 | ||
Modular Common Spacecraft Bus | United States | NASA Ames Research Center | } | 1 | Operational | 2013 LADEE | Very low-cost bus, capable of Lunar, Asteroidal, and Earth orbit missions.[7] | |||
RS-300 | United States | Ball Aerospace | <125 kg[8] | 0 | Operational (as of 2009[update]) |
RS-300 | ||||
I-1K | India | Antrix Corporation | <1,300 kg[9] | Operational | I-1000, Ideal for most small communication and meteorological satellites | |||||
I-2K | India | Antrix Corporation | 1,540 kg - 2,800 kg[10] | Operational | I-2000,ideal for most of medium level communication payloads | |||||
I-3K | India | Antrix Corporation | >3,000 kg[11] | 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 | Development | I-4000 | |||||
SI-100 | Korea | Satrec | 100 kg[12] | Development | SI-100 | |||||
SI-200 | Korea | Satrec | 200 kg[13] | Operational | SI-200 | |||||
SI-300 | Korea | Satrec | 300 kg[14] | ? | SI-300 | |||||
SNC-100 | United States | SNC Space Systems | 100 kg[15] | 0 | Development | 2013 | SNC-100 | |||
SNC-100-L1 | United States | SNC Space Systems | 100 kg[16] | 0 | Development | Optimized for LauncherOne[16] | ||||
Spacebus 100 | France | Thales Alenia Space | 1,170 kg[6] | 3 | Operational[17] | 1985[6] | [note 1] | GEO; used for Arabsat-1A | ||
Spacebus 300 | France | Thales Alenia Space | 5 | Operational | 1987 | 1990 | GEO | |||
Spacebus 2000 | France | Thales Alenia Space | 11 | Operational | 1990 | 1998 | GEO | |||
Spacebus 3000 | France | Thales Alenia Space | 27 | Operational | 1996 | 2010 | GEO | |||
Spacebus 4000 | France | Thales Alenia Space | 29 | Operational | 2005 | 2012 | GEO | |||
SpaceEye-1 | Korea | Satrec | 300 kg[14] | ? | SpaceEye-1 | |||||
SpaceEye-2 | Korea | Satrec | 200 kg[14] | ? | SpaceEye-2 | |||||
SpaceEye-10 | Korea | Satrec | 100 kg[14] | ? | SpaceEye-10 | |||||
SSTL-100LO | United Kingdom | Surrey Satellite Technology | 100 kg[16] | 0 | Development | Optimized for LauncherOne[16] |
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
- ^ Eric Anderson (30 Aug 2012). Eric Anderson – The Arkyd Series (video interview). moonandback.com. Retrieved 2012-09-06.
- ^ a b c d e f g
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
- ^ a b c Krebs, Gunter. "Hughes: HS-333 / HS-356". Gunter's Space Page. Retrieved 4 July 2012.
- ^ a b c d "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).
- ^ 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.
- ^ "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.
- ^ 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.
- ^ a b c d "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 [are] in production
- ^ a b c d
"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)
Notes
- ^ It is not clear from the sources if the Spacebus 100 satellite bus is still on offer.