USP (satellite bus)

USP (УКП)
Manufacturer RSC Energia
Country of origin Russia
Applications Communications,
Specifications
Spacecraft type LEO to GEO universal platform
Design life HEO >= 7 years
GEO >=12.5 years
Dry mass 950 kg (2,090 lb) to 1,200 kg (2,600 lb)
Payload capacity HEO: 500 kg (1,100 lb) to 1,000 kg (2,200 lb)
GEO 250 kg (550 lb) to 300 kg (660 lb)
Power HEO up to 3000W
GEO up to 2000W
Batteries NiH2
Regime LEO, HEO and GEO
Production
Status In Prduction
Built 7
On order 12
Launched 6
Operational 2
Retired 1
Failed 2
Lost 1
First launch September 06, 1999, Yamal 101 and Yamal 102
Last launch November 17, 2015, Tundra L11

The USP, for Universal Space Platform (Russian: УКП, Универсальная Космическая Платформа), also known as Viktoria (Викториа), is a highly flexible satellite bus designed and manufactured by RSC Energia.[1][2][3][4][5][6] It is called universal because it has been designed to be operated from LEO to GEO.[1] It is a three axis stabilized platform with electric propulsion for station keeping, but chemical propellant is offered as an option.[1] The bus can offer up to 3000 W of power and a payload capacity up to 1,000 kg (2,200 lb) for Low Earth orbit or HEO an up to 300 kg (660 lb) for geostationary orbit.[1]

The platform is designed for direct orbital injection, and thus lacks orbit raising propulsion.[3] It does however, support dual launching on Proton-M, which can enable cheap launching, or the use of smaller vehicles like the Soyuz-2.1b/Fregat-M or even the Dnepr for low energy orbits.[1]

List of USP bus satellites

While not the most successful satellite bus, the USP is characterized by its commercial beginnings and the huge orbital flexibility.

Satellite Order Launch Launch Vehicle Launch Site Intended Orbit Launch Result Launch Weight Status Remarks
Yamal 101 N/A 1999-09-06 Proton-K/Blok-DM-2M Baikonur Site 81/23 GEO Success 1,360 kg (3,000 lb) Failed at separation Dual launch with Yamal 102. Failed at launch [7][8][9][10][11]
Yamal 102 N/A 1999-09-06 Proton-K/Blok-DM-2M Baikonur Site 81/23 GEO Success 1,360 kg (3,000 lb) Retired on August 9, 2010 Dual launch with Yamal 101. [7][8][9][10]
Yamal 201 2001 2003-11-24 Proton-K/Blok-DM-2M Baikonur Site 81/23 GEO Success 1,360 kg (3,000 lb) Failed on June 5, 2014 Dual launch with Yamal 202. Failed on orbit[12][13][14][8][15][16][17][18]
Yamal 202 2001 2003-11-24 Proton-K/Blok-DM-2M Baikonur Site 81/23 GEO Success 1,320 kg (2,910 lb) Operational Dual launch with Yamal 201[19][20][8][15][16][17][21]
BelKa 1 2003 2006-07-26 Dnepr/Blok-DM-2M Baikonur Site 109/95 SSO Failure 750 kg (1,650 lb) Launch failure [22][23][24]
Tundra L11 2007 2015-11-17 Soyuz-2.1b/Fregat-M Plesetsk Site 43/4 HEO Success N/A Operational [25][26]
Tundra L12 2007 2016 Soyuz-2.1b/Fregat-M Plesetsk Site 43/4 HEO 2016 N/A Planned [25][27]
Angosat 1 2017 Angara A5/Blok DM-03 Plesetsk Site 35/1 GEO 2017 1,550 kg (3,420 lb) Planned [28][6][29]
Tundra L13 2007 2017 Soyuz-2.1b/Fregat-M Plesetsk Site 43/4 HEO 2017 N/A Planned [25][27]
Energia-100 2018 Soyuz-2.1b/Fregat-M Vostochny Site 1SGEO 2018 N/A Planned [30][6]
Tundra L14 2007 2019 Soyuz-2.1b/Fregat-M Plesetsk Site 43/4 HEO 2019 N/A Planned [25][27]
Tundra L15 2007 2020 Soyuz-2.1b/Fregat-M Plesetsk Site 43/4 HEO 2020 N/A Planned [25][27]
Yamal 203 2001 Cancelled Proton-K/Blok-DM-2M Baikonur GEO Cancelled 1,360 kg (3,000 lb) Cancelled [6][12][8][16][17]
Yamal 204 2001 Cancelled Proton-K/Blok-DM-2M Baikonur GEO Cancelled 1,320 kg (2,910 lb) Cancelled [6][19][8][16][17]
Yamal 301 2003 Cancelled Proton-M/Blok DM-03 Baikonur GEO Cancelled 1,330 kg (2,930 lb) Cancelled [6][31][8][32]
Yamal 302 2003 Cancelled Proton-M/Blok DM-03 Baikonur GEO Cancelled 1,330 kg (2,930 lb) Cancelled [6][33][8][32]

See also

RSC Energia USP page

References

  1. 1 2 3 4 5 "Universal Space Platform". RSC Energia. Retrieved 2016-07-20.
  2. ↑ "YAMAL-200 Communications Satellite". RSC Energia. Retrieved 2016-07-20.
  3. 1 2 "YAMAL-200 Communications Satellite Satellite Components". RSC Energia. Retrieved 2016-07-20.
  4. ↑ "YAMAL-200 Communications Satellite Bus Module". RSC Energia. Retrieved 2016-07-20.
  5. ↑ "YAMAL-200 Communications Satellite Payload module". RSC Energia. Retrieved 2016-07-20.
  6. 1 2 3 4 5 6 7 Krebs, Gunter Dirk (2015-10-16). "RKK Energiya: USP (Victoria)". Gunter's Space Page. Retrieved 2016-07-20.
  7. 1 2 Krebs, Gunter Dirk (2016-04-17). "Yamal 101, 102". Gunter's Space Page. Retrieved 2016-07-20.
  8. 1 2 3 4 5 6 7 8 Zak, Anatoly (April 21, 2016). "Yamal communication satellites". RussiaSpaceWeb.com. Retrieved 2016-07-20.
  9. 1 2 Pillet, Nicolas. "Yamal/Historie/Nécessité de renouvellement" [Yamal/History/The necessity of renewal]. Kosmonavtika (in French). Retrieved 2016-07-20.
  10. 1 2 Pillet, Nicolas. "Yamal/Historie/La plate-forme universelle" [Yamal/History/The universal platform]. Kosmonavtika (in French). Retrieved 2016-07-20.
  11. ↑ "Yamal 101". Satbeams. Retrieved 20 July 2016.
  12. 1 2 Krebs, Gunter Dirk (2016-04-17). "Yamal 201, 203". Gunter's Space Page. Retrieved 2016-07-20.
  13. ↑ "Russian satellite failure leads to channels move". DigitalTVEurope.NET. June 9, 2014. Retrieved 2016-07-20.
  14. ↑ Todd, David (June 10, 2014). "Yamal 201 may have failed in orbit as customers are moved to other satellites". Seradata Space Intelligence. Retrieved 2016-07-20.
  15. 1 2 Zak, Anatoly (March 9, 2016). "Proton missions in 2003". RussiaSpaceWeb.com. Retrieved 2016-07-20.
  16. 1 2 3 4 Pillet, Nicolas. "Yamal/Historie/Premier tir, premier revers" [Yamal/History/The first setbacks]. Kosmonavtika (in French). Retrieved 2016-07-20.
  17. 1 2 3 4 Pillet, Nicolas. "Yamal/Historie/La deuxième génération" [Yamal/History/The second generation]. Kosmonavtika (in French). Retrieved 2016-07-20.
  18. ↑ "Yamal 201". Satbeams. Retrieved 20 July 2016.
  19. 1 2 Krebs, Gunter Dirk (2016-04-17). "Yamal 202, 204". Gunter's Space Page. Retrieved 2016-07-20.
  20. ↑ "Yamal-202 technical performance". Gazprom Space Systems. Retrieved 2016-07-20.
  21. ↑ "Yamal 201". Satbeams. Retrieved 20 July 2016.
  22. ↑ Krebs, Gunter Dirk (2016-04-17). "BelKa 1". Gunter's Space Page. Retrieved 2016-07-20.
  23. ↑ Zak, Anatoly (December 17, 2012). "BelKA". RussiaSpaceWeb.com. Retrieved 2016-07-20.
  24. ↑ Pillet, Nicolas. "Le satellite BelKA/Historique" [The history of the BelKa satellite]. Kosmonavtika (in French). Retrieved 2016-07-20.
  25. 1 2 3 4 5 Krebs, Gunter Dirk (2016-04-17). "Tundra (EKS, 14F142)". Gunter's Space Page. Retrieved 2016-07-20.
  26. ↑ Zak, Anatoly (December 7, 2015). "First launch into the EKS constellation". RussiaSpaceWeb.com. Retrieved 2016-07-20.
  27. 1 2 3 4 Zak, Anatoly (November 19, 2015). "Development of the EKS system". RussiaSpaceWeb.com. Retrieved 2016-07-20.
  28. ↑ Krebs, Gunter Dirk (2016-04-17). "AngoSat 1". Gunter's Space Page. Retrieved 2016-07-20.
  29. ↑ "Angosat 1". Satbeams. Retrieved 19 July 2016.
  30. ↑ "Спутник "Энергия-100" планируют запустить с "Восточного" в 2018 году" [Energia-100 satellite planned for a 2018 launch from Vostochny] (in Russian). Ria Novosti. October 6, 2015. Retrieved 2016-07-20.
  31. ↑ Krebs, Gunter Dirk (2016-04-17). "Yamal 301". Gunter's Space Page. Retrieved 2016-07-20.
  32. 1 2 Pillet, Nicolas. "Yamal/Historie/Les Yamal-300" [Yamal/History/The Yamal-300]. Kosmonavtika (in French). Retrieved 2016-07-20.
  33. ↑ Krebs, Gunter Dirk (2016-04-17). "Yamal 302". Gunter's Space Page. Retrieved 2016-07-20.
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