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USP (satellite bus)

The USP, for Universal Space Platform (Russian: УКП, Универсальная Космическая Платформа), also known as Viktoria (Виктория), 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]

USP (УКП)
ManufacturerRSC Energia
Country of originRussia
ApplicationsCommunications,
Specifications
Spacecraft typeLEO to GEO universal platform
Dry mass950 kg (2,090 lb) to 1,200 kg (2,600 lb)
Payload capacityHEO: 500 kg (1,100 lb) to 1,000 kg (2,200 lb)
GEO 250 kg (550 lb) to 300 kg (660 lb)
PowerHEO up to 3000W
GEO up to 2000W
BatteriesNiH2
RegimeLEO, HEO and GEO
Design lifeHEO >= 7 years
GEO >=12.5 years
Production
StatusIn Production
On order12
Built7
Launched7
Operational3
Retired1
Failed2
Lost1
Maiden launchSeptember 06, 1999, Yamal 101 and Yamal 102
Last launchDec 26, 2017, Angosat 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 edit

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 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 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 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 Operational [25][26]
Tundra L12 2007 2017-05-25 Soyuz-2.1b/Fregat-M Plesetsk Site 43/4 HEO Success Operational [25][27]
Angosat 1 2009 2017-12-26 Zenit-3F/Fregat-SB Baikonur Site 45/1 GEO Success 1,550 kg (3,420 lb) Commissioning The ground controllers lose contact with the satellite shortly after launch, but later regained after the satellite was properly aligned with sun and confirmed that its onboard systems are in good health.[28][29][6][30]
Tundra L13 2007 2018 Soyuz-2.1b/Fregat-M Plesetsk Site 43/4 HEO 2018 Planned [25][27]
Energia-100 2018 Soyuz-2.1b/Fregat-M Vostochny Site 1S GEO 2018 Planned [31][6]
Tundra L14 2007 2019 Soyuz-2.1b/Fregat-M Plesetsk Site 43/4 HEO 2019 Planned [25][27]
Tundra L15 2007 2020 Soyuz-2.1b/Fregat-M Plesetsk Site 43/4 HEO 2020 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][32][8][33]
Yamal 302 2003 Cancelled Proton-M/Blok DM-03 Baikonur GEO Cancelled 1,330 kg (2,930 lb) Cancelled [6][34][8][33]

See also edit

External links edit

References edit

  1. ^ a b c d e . RSC Energia. Archived from the original on 2016-06-17. Retrieved 2016-07-20.
  2. ^ . RSC Energia. Archived from the original on 2016-06-17. Retrieved 2016-07-20.
  3. ^ a b . RSC Energia. Archived from the original on 2016-06-04. Retrieved 2016-07-20.
  4. ^ . RSC Energia. Archived from the original on 2016-06-09. Retrieved 2016-07-20.
  5. ^ . RSC Energia. Archived from the original on 2016-06-09. Retrieved 2016-07-20.
  6. ^ a b c d e f g Krebs, Gunter Dirk (2015-10-16). "RKK Energiya: USP (Victoria)". Gunter's Space Page. Retrieved 2016-07-20.
  7. ^ a b Krebs, Gunter Dirk (2016-04-17). "Yamal 101, 102". Gunter's Space Page. Retrieved 2016-07-20.
  8. ^ a b c d e f g h Zak, Anatoly (April 21, 2016). "Yamal communication satellites". RussiaSpaceWeb.com. Retrieved 2016-07-20.
  9. ^ a b Pillet, Nicolas. [Yamal/History/The necessity of renewal]. Kosmonavtika (in French). Archived from the original on 2016-08-19. Retrieved 2016-07-20.
  10. ^ a b Pillet, Nicolas. [Yamal/History/The universal platform]. Kosmonavtika (in French). Archived from the original on 2016-08-19. Retrieved 2016-07-20.
  11. ^ "Yamal 101". Satbeams. Retrieved 20 July 2016.
  12. ^ a b 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). . Seradata Space Intelligence. Archived from the original on 2016-09-21. Retrieved 2016-07-20.
  15. ^ a b Zak, Anatoly (March 9, 2016). "Proton missions in 2003". RussiaSpaceWeb.com. Retrieved 2016-07-20.
  16. ^ a b c d Pillet, Nicolas. [Yamal/History/The first setbacks]. Kosmonavtika (in French). Archived from the original on 2016-08-19. Retrieved 2016-07-20.
  17. ^ a b c d Pillet, Nicolas. [Yamal/History/The second generation]. Kosmonavtika (in French). Archived from the original on 2016-08-19. Retrieved 2016-07-20.
  18. ^ "Yamal 201". Satbeams. Retrieved 20 July 2016.
  19. ^ a b 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. [The history of the BelKa satellite]. Kosmonavtika (in French). Archived from the original on 2016-08-20. Retrieved 2016-07-20.
  25. ^ a b c d e 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. ^ a b c d Zak, Anatoly (November 19, 2015). "Development of the EKS system". RussiaSpaceWeb.com. Retrieved 2016-07-20.
  28. ^ Henry, Caleb (29 December 2017). "Angosat-1 communications restored after post-launch glitch - SpaceNews.com". SpaceNews.com. Retrieved 29 December 2017.
  29. ^ Krebs, Gunter Dirk (2016-04-17). "AngoSat 1". Gunter's Space Page. Retrieved 2016-07-20.
  30. ^ "Angosat 1". Satbeams. Retrieved 19 July 2016.
  31. ^ "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.
  32. ^ Krebs, Gunter Dirk (2016-04-17). "Yamal 301". Gunter's Space Page. Retrieved 2016-07-20.
  33. ^ a b Pillet, Nicolas. [Yamal/History/The Yamal-300]. Kosmonavtika (in French). Archived from the original on 2016-08-19. Retrieved 2016-07-20.
  34. ^ Krebs, Gunter Dirk (2016-04-17). "Yamal 302". Gunter's Space Page. Retrieved 2016-07-20.

satellite, universal, space, platform, russian, УКП, Универсальная, Космическая, Платформа, also, known, viktoria, Виктория, highly, flexible, satellite, designed, manufactured, energia, called, universal, because, been, designed, operated, from, three, axis, . The USP for Universal Space Platform Russian UKP Universalnaya Kosmicheskaya Platforma also known as Viktoria Viktoriya 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 USP UKP ManufacturerRSC EnergiaCountry of originRussiaApplicationsCommunications SpecificationsSpacecraft typeLEO to GEO universal platformDry mass950 kg 2 090 lb to 1 200 kg 2 600 lb Payload capacityHEO 500 kg 1 100 lb to 1 000 kg 2 200 lb GEO 250 kg 550 lb to 300 kg 660 lb PowerHEO up to 3000W GEO up to 2000WBatteriesNiH2RegimeLEO HEO and GEODesign lifeHEO gt 7 years GEO gt 12 5 yearsProductionStatusIn ProductionOn order12Built7Launched7Operational3Retired1Failed2Lost1Maiden launchSeptember 06 1999 Yamal 101 and Yamal 102Last launchDec 26 2017 Angosat 1The 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 Contents 1 List of USP bus satellites 2 See also 3 External links 4 ReferencesList of USP bus satellites editWhile 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 RemarksYamal 101 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 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 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 Operational 25 26 Tundra L12 2007 2017 05 25 Soyuz 2 1b Fregat M Plesetsk Site 43 4 HEO Success Operational 25 27 Angosat 1 2009 2017 12 26 Zenit 3F Fregat SB Baikonur Site 45 1 GEO Success 1 550 kg 3 420 lb Commissioning The ground controllers lose contact with the satellite shortly after launch but later regained after the satellite was properly aligned with sun and confirmed that its onboard systems are in good health 28 29 6 30 Tundra L13 2007 2018 Soyuz 2 1b Fregat M Plesetsk Site 43 4 HEO 2018 Planned 25 27 Energia 100 2018 Soyuz 2 1b Fregat M Vostochny Site 1S GEO 2018 Planned 31 6 Tundra L14 2007 2019 Soyuz 2 1b Fregat M Plesetsk Site 43 4 HEO 2019 Planned 25 27 Tundra L15 2007 2020 Soyuz 2 1b Fregat M Plesetsk Site 43 4 HEO 2020 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 32 8 33 Yamal 302 2003 Cancelled Proton M Blok DM 03 Baikonur GEO Cancelled 1 330 kg 2 930 lb Cancelled 6 34 8 33 See also editRSC Energia The USP bus designer and manufacturer Gazprom Space Systems Satellite communication division of the Russian oil giant Gazprom Yamal Communication satellite family operated by Gazprom Space Systems EKS early warning system A Russian early warning satellite system designed by RSC Energia that is based on the USP bus External links editRSC Energia USP page Archived 2016 06 17 at the Wayback MachineReferences edit a b c d e Universal Space Platform RSC Energia Archived from the original on 2016 06 17 Retrieved 2016 07 20 YAMAL 200 Communications Satellite RSC Energia Archived from the original on 2016 06 17 Retrieved 2016 07 20 a b YAMAL 200 Communications Satellite Satellite Components RSC Energia Archived from the original on 2016 06 04 Retrieved 2016 07 20 YAMAL 200 Communications Satellite Bus Module RSC Energia Archived from the original on 2016 06 09 Retrieved 2016 07 20 YAMAL 200 Communications Satellite Payload module RSC Energia Archived from the original on 2016 06 09 Retrieved 2016 07 20 a b c d e f g Krebs Gunter Dirk 2015 10 16 RKK Energiya USP Victoria Gunter s Space Page Retrieved 2016 07 20 a b Krebs Gunter Dirk 2016 04 17 Yamal 101 102 Gunter s Space Page Retrieved 2016 07 20 a b c d e f g h Zak Anatoly April 21 2016 Yamal communication satellites RussiaSpaceWeb com Retrieved 2016 07 20 a b Pillet Nicolas Yamal Historie Necessite de renouvellement Yamal History The necessity of renewal Kosmonavtika in French Archived from the original on 2016 08 19 Retrieved 2016 07 20 a b Pillet Nicolas Yamal Historie La plate forme universelle Yamal History The universal platform Kosmonavtika in French Archived from the original on 2016 08 19 Retrieved 2016 07 20 Yamal 101 Satbeams Retrieved 20 July 2016 a b Krebs Gunter Dirk 2016 04 17 Yamal 201 203 Gunter s Space Page Retrieved 2016 07 20 Russian satellite failure leads to channels move DigitalTVEurope NET June 9 2014 Retrieved 2016 07 20 Todd David June 10 2014 Yamal 201 may have failed in orbit as customers are moved to other satellites Seradata Space Intelligence Archived from the original on 2016 09 21 Retrieved 2016 07 20 a b Zak Anatoly March 9 2016 Proton missions in 2003 RussiaSpaceWeb com Retrieved 2016 07 20 a b c d Pillet Nicolas Yamal Historie Premier tir premier revers Yamal History The first setbacks Kosmonavtika in French Archived from the original on 2016 08 19 Retrieved 2016 07 20 a b c d Pillet Nicolas Yamal Historie La deuxieme generation Yamal History The second generation Kosmonavtika in French Archived from the original on 2016 08 19 Retrieved 2016 07 20 Yamal 201 Satbeams Retrieved 20 July 2016 a b Krebs Gunter Dirk 2016 04 17 Yamal 202 204 Gunter s Space Page Retrieved 2016 07 20 Yamal 202 technical performance Gazprom Space Systems Retrieved 2016 07 20 Yamal 201 Satbeams Retrieved 20 July 2016 Krebs Gunter Dirk 2016 04 17 BelKa 1 Gunter s Space Page Retrieved 2016 07 20 Zak Anatoly December 17 2012 BelKA RussiaSpaceWeb com Retrieved 2016 07 20 Pillet Nicolas Le satellite BelKA Historique The history of the BelKa satellite Kosmonavtika in French Archived from the original on 2016 08 20 Retrieved 2016 07 20 a b c d e Krebs Gunter Dirk 2016 04 17 Tundra EKS 14F142 Gunter s Space Page Retrieved 2016 07 20 Zak Anatoly December 7 2015 First launch into the EKS constellation RussiaSpaceWeb com Retrieved 2016 07 20 a b c d Zak Anatoly November 19 2015 Development of the EKS system RussiaSpaceWeb com Retrieved 2016 07 20 Henry Caleb 29 December 2017 Angosat 1 communications restored after post launch glitch SpaceNews com SpaceNews com Retrieved 29 December 2017 Krebs Gunter Dirk 2016 04 17 AngoSat 1 Gunter s Space Page Retrieved 2016 07 20 Angosat 1 Satbeams Retrieved 19 July 2016 Sputnik Energiya 100 planiruyut zapustit s Vostochnogo v 2018 godu Energia 100 satellite planned for a 2018 launch from Vostochny in Russian Ria Novosti October 6 2015 Retrieved 2016 07 20 Krebs Gunter Dirk 2016 04 17 Yamal 301 Gunter s Space Page Retrieved 2016 07 20 a b Pillet Nicolas Yamal Historie Les Yamal 300 Yamal History The Yamal 300 Kosmonavtika in French Archived from the original on 2016 08 19 Retrieved 2016 07 20 Krebs Gunter Dirk 2016 04 17 Yamal 302 Gunter s Space Page Retrieved 2016 07 20 Retrieved from https en wikipedia org w index php title USP satellite bus amp oldid 1142238581, wikipedia, wiki, book, books, library,

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