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सोयुज-2
Reference material by Wikipedia contributors. This retains its source identity and is not 411 news reporting.
Soyuz 2 metop.jpg सोयुज-2.1ए रॉकेट. सोयुज-2 (2.1ए /2.1बी /एसटी-ए /एसटी-बी) वाहक रॉकेट TsSKB-Progress 46.3 m onhttp://en.samspace.ru/products/launch_vehicles/rn_soyuz_2/ SOYUZ-2 Launch Vehicle / Power Characteristics JSC SRC Progress 2015-08-20 https://web.archive.org/web/20161221052518/http://en.samspace.ru/products/launch_vehicles/rn_soyuz_2/ 21 दिसंबर 2016 dead 2.95 m on 312,000 kg on 2 or 3 LEO200 km nmi on circular LEO 51.8° inclination from Baikonur
2.1a: 7020 kg on2.1b: 8200 kg on
SSO820 km nmi on SSO (with Fregat from Kourou)
ST-A: 4230 kg onST-B: 4900 kg on
GTO1500 m/s on ΔV deficit GTO (with Fregat from Kourou)
ST-A: 2810 kg onST-B: 3250 kg on
R-7 (Soyuz) Active Baikonur Site 31/6
Plesetsk Site 43
Kourou ELS
Vostochny Site 1S 62 (2.1a: 28, 2.1b: 32, 2.1v: 2) 57 (2.1a: 26, 2.1b: 30, 2.1v: 1) 2 (2.1a: 1, 2.1b: 1, 2.1v: 0) 3 (2.1a: 1, 2.1b: 1, 2.1v: 1) 2.1a: 8 November 20042.1b: 27 December 20062.1v: 28 December 2013 CoRoT
Galileo
GLONASS
Progress
booster
Blok-B,V,G,Dhttp://www.arianespace.com/wp-content/uploads/2015/09/Soyuz-Users-Manual-March-2012.pdf Soyuz from the Guiana Space Centre - User's manual 2 PDF Arianespace March 2012 16 December 2015 https://web.archive.org/web/20180403120245/http://www.arianespace.com/wp-content/uploads/2015/09/Soyuz-Users-Manual-March-2012.pdf 3 अप्रैल 2018 dead
4
19.6 m ft on
2.68 m ft on
3784 kg on
44413 kg on
39160 kg on
RD-107A
Sea level: 839.48 kN onVacuum: 1019.93 kN on
Sea level: 263.3 isp onVacuum: 320.2 isp on
118 seconds
LOX / RG-1
stage
First
Blok-A
27.10 m ft on
2.95 m ft on
6545 kg on
99765 kg on
90100 kg on
RD-108A
Sea level: 792.41 kN onVacuum: 921.86 kN on
Sea level: 257.7 isp onVacuum: 320.6 isp on
286 seconds
LOX / RG-1
stage
Second
Blok-I
6.70 m on
2.66 m on
2355 kg on
27755 kg on
25400 kg on
2.1a / STA: RD-01102.1b / STB: RD-0124
RD-0110: 298 kN onRD-0124: 294.3 kN on
RD-0110: 326 secondsRD-0124: 359 seconds
270 seconds
LOX / RG-1
stage
optional
Upper
Fregat / Fregat-M / Fregat-MTКонструкция разгонного блока "Фрегат" http://www.laspace.ru/rus/fregat_construction.php NPO Lavochkin 10 March 2016 ru https://web.archive.org/web/20151226122333/http://www.laspace.ru/rus/fregat_construction.php 26 दिसंबर 2015 live
1.5 m ft on
Fregat / Fregat-M: 3.35 m ft onFregat-MT: 3.80 m ft on
Fregat: 930 kg onFregat-M: 980 kg onFregat-MT: 1050 kg on
Fregat: 5250 kg onFregat-M: 5600 kg onFregat-MT: 7100 kg on
S5.92
19.85 kN on
333.2 seconds
1100 seconds
N2O4 / UDMH
stage
optional
Upper
VolgaVolga upper stage http://russianspaceweb.com/volga.html Russianspaceweb.com 10 March 2016 https://web.archive.org/web/20160304041508/http://www.russianspaceweb.com/volga.html 4 मार्च 2016 live
1.025 m ft on
3.2 m ft on
840 kg on
300-900 kg on
17D64https://www.nasaspaceflight.com/2016/04/vostochny-maiden-soyuz-launch/ Soyuz 2-1 launches maiden mission from Vostochny NASASpaceFlight.com www.nasaspaceflight.com 2016-05-01 https://web.archive.org/web/20170128130218/https://www.nasaspaceflight.com/2016/04/vostochny-maiden-soyuz-launch/ 28 जनवरी 2017 live
2.94 kN on
307 seconds
N2O4 / UDMH
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