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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			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 United Kingdom Germany	EADS Astrium		6,400 kg		40+	Operational	1990		GEO
HS-333	United States	Hughes Space and Communications	54 kg	560		8	Retired	1972	1979	GEO; first satellite series; eight built, 300 watt, 12-channel, single-antenna
LS-1300	United States	Space Systems/Loral		5,500–6700 kg		> 30	Operational	1984	2012	GEO; previously named the FS-1300
RS-300	United States	Ball Aerospace		<125 kg		0	Operational (as of 2009)			RS-300
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			Development			I-4000
SI-100	South Korea	Satrec		100 kg			Development			SI-100
SI-200	South Korea	Satrec		200 kg			Operational			SI-200
SI-300	South 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	Operational	1985		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	South Korea	Satrec		300 kg			?			SpaceEye-1
SpaceEye-2	South Korea	Satrec		200 kg			?			SpaceEye-2
SpaceEye-10	South Korea	Satrec		100 kg			?			SpaceEye-10
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

Template:Multicol-end

See also

• Launch vehicle
• Product model

References

1. Eric Anderson (30 Aug 2012). Eric Anderson – The Arkyd Series (video interview). moonandback.com. Retrieved 2012-09-06.
2. ^ Werner, Debra (2012-08-13). "Builder Packing More Capability into Small Satellites". Space News. p. 13. {{cite news}}: |access-date= requires |url= (help)
3. "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
4. Hughes Aircraft Corporation, Space and Communications Group, SBS F6 Prime sales brochure, 1985
5. ^ Krebs, Gunter. "Hughes: HS-333 / HS-356". Gunter's Space Page. Retrieved 4 July 2012.
6. ^ "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).
7. Krebs, Gunter. "Ball: RS-300". Gunter's Space Page. Retrieved 21 March 2011.
8. "SPACECRAFT SYSTEMS AND SUB SYSTEMS". Antrix Corporation. Retrieved 2013-02-02.
9. "SPACECRAFT SYSTEMS AND SUB SYSTEMS". Antrix Corporation. Retrieved 2013-02-02.
10. "SPACECRAFT SYSTEMS AND SUB SYSTEMS". Antrix Corporation. Retrieved 2013-02-02.
11. Wade, Mark. "Satrec". Encyclopedia Astronautica. Retrieved 2012-09-16.
12. Krebs, Gunter (2012-02-09). "Satrec Initiative: SI-200". Skyrocket.de (Gunter's Space Page). Retrieved 2012-09-16.
13. ^ "Satellite System Products". Satrec Initiative. 2012. Retrieved 2012-09-16.
14. "SN-100 Small Satellite Production Line". Space News. 2012-08-13. p. 21. first 18 satellites in production
15. ^ "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).
16. 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

1. It is not clear from the sources if the Spacebus 100 satellite bus is still on offer.

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