Jump to content

Comparison of orbital launch systems

From Wikipedia, the free encyclopedia

This is an old revision of this page, as edited by Fm3dici97 (talk | contribs) at 11:26, 1 December 2022 (→Current rockets: Updated Soyuz-2.1b stats). The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.

A Falcon Heavy launch vehicle from SpaceX

This comparison of orbital launch systems lists the attributes of all individual rocket configurations designed to reach orbit. A first list contains rockets that are currently operational or in development; a second list includes all retired rockets. For the simple list of all conventional launcher families, see: Comparison of orbital launchers families. For the list of predominantly solid-fueled orbital launch systems, see: Comparison of solid-fueled orbital launch systems.

Spacecraft propulsion[note 1] is any method used to accelerate spacecraft and artificial satellites. A conventional solid rocket or a conventional solid-fuel rocket is a rocket with a motor that uses solid propellants (fuel/oxidizer).[note 2] Orbital launch systems are rockets and other systems capable of placing payloads into or beyond Earth orbit. All current spacecraft use conventional chemical rockets (bipropellant or solid-fuel) for launch, though some[note 3] have used air-breathing engines on their first stage.[note 4]

Current rockets

Orbits legend:

Vehicle Origin Manufacturer Payload mass to ... (kg) Orbital launches incl. failures[a] Date of flight
LEO GTO Other First Latest
Alpha  United States Firefly Aerospace 1,000[1] 630 to SSO 2 2021 2022
Angara A5  Russia Khrunichev 24,000[2] 5,400 with Briz-M[2]
7,500 with KVTK 		3[3] 2014 2021
Angara 1.2  Russia Khrunichev 3,500[2] 2,400 to SSO 2[4] 2022 2022
Antares 230 / 230+  United States Northrop Grumman 8,200[5] 3,000 to SSO[b] 6[6] 2016 2021
Ariane 5 (all variants)  Europe EADS Astrium (Arianegroup) 21,000[7] 11,210[8] 113 1996 2022
Atlas V 551  United States ULA 18,500[9] 8,700 13,550 to SSO
3,960 to GEO 		12[9] 2006 2021
Atlas V N22[c]  United States ULA 13,000 2 2019[11] 2022
Ceres-1  China Galactic Energy 350 270 to SSO 4[12] 2020 2022
Delta IV Heavy  United States ULA 28,790[13] 14,220 23,560 to polar
11,290 to TLI
8,000 to TMI 		14[14] 2004 2022
Electron  United States
 New Zealand 		Rocket Lab 300[15] 200 to SSO[15] 26[16] 2017 2022
Epsilon  Japan IHI[17] 1,500[18] 590 to SSO 6[19] 2013 2019
Falcon 9 Full Thrust
(partially reusable) 		 United States SpaceX 16,800+[20] 5,500[21][d] 9,600 to polar[23] 351[24][25][e] 2015 2022
Falcon 9 Full Thrust
(expended) 		 United States SpaceX 22,800[21] 8,300[21] 4,020 to TMI 16[27][28] 2017 2022
Falcon Heavy
(partially reusable)[29] 		 United States SpaceX 30,000[30]–57,000[31] 8,000[21]–10,000[f] 11[32][33] 2018 2022
Falcon Heavy
(expended) 		 United States SpaceX 63,800[34] 26,700[34] 16,800 to TMI[34] 0 – [g]
GSLV Mk II  India ISRO 5,000[35] 2,700[36][h] 7[37] 2010 2018
GSLV Mk III  India ISRO 10,000[38] 4,000 2,380 to TLI 3[39] 2017[i] 2022[j]
H-IIA 202  Japan Mitsubishi 8,000[42]: 67  4,000[42]: 48  5,100 to SSO[k]
[42]: 64–65  		26[43] 2001 2020
Hyperbola-1  China i-Space 300[44] 4[45] 2019[46][l] 2022
Jielong 1[47]  China CALT 200 (SSO) 1[47] 2019 2019
Kaituozhe-2  China CASC 800[48] 1[48] 2017 2017
Kuaizhou 1/1A  China ExPace 400[49] 15[49] 2013[m] 2022
Kuaizhou 11  China ExPace 1,500[50] 1,000 to SSO[51] 1 2020 2020
LauncherOne  United States Virgin Orbit 500[52] 300 to SSO[53] 4 2020 2022
Lijian-1 (ZhongKe-1A)  China CAS Space 2,000[54] 1,500[55] TO 500 km SSO 1[56] 2022 2022
Long March 2C  China CALT 3,850
[citation needed] 		1,250 with CTS2 2,000 to SSO with YZ-1S[57] 64[58] 1982 2022
Long March 2D  China SAST 4,000 1,150 to SSO 70[58] 1992 2022
Long March 2F  China CALT 8,600 19[58] 1999 2022
Long March 3A  China CALT 6,000[59] 2,600 5,000 to SSO 27[60] 1994 2018
Long March 3B/E  China CALT 11,500[59] 5,500 6,900 to SSO 67[60] 2007 2022
Long March 3C  China CALT 9,100[59] 3,800 6,500 to SSO 18[60] 2008 2021
Long March 4B  China SAST 4,200[61] 1,500 2,800 to SSO 43[61] 1999 2021
Long March 4C  China SAST 4,200[62] 1,500 2,800 to SSO 46[61] 2006 2022
Long March 5  China CALT 14,000 [63] 15,000 to SSO[64]
9,400 to TLI[63]
6,000 to TMI[63] 		5[64] 2016 2020
Long March 5B  China CALT 25,000[64] 3[64] 2020[65] 2022
Long March 6  China SAST 1,080 to SSO[66] 8[67] 2015 2021
Long March 6A  China SAST 4,000 to SSO[68] 2[67] 2022 2022
Long March 7  China CALT 13,500[69] 5,500 to SSO 6[70] 2016[71] 2021
Long March 7A  China CALT 5,500 to 7,000[65] 3[70] 2020 2021
Long March 8  China CALT 8,400 2,800 5,000 to SSO 2[72] 2020 2022
Long March 11  China CALT 700[73] 350 to SSO 13[74] 2015 2022
Minotaur I  United States Northrop Grumman 580[75] 12[76] 2000 2021
Minotaur IV  United States Northrop Grumman 1,735[77] 5[78][n] 2010 2020
Minotaur V  United States Northrop Grumman 670[78] 465 to HCO 1[78] 2013 2013
Minotaur-C (Taurus)[79]  United States Northrop Grumman 1,458[80] 1,054 to SSO[o] 10[81] 1994 2017
Nuri (KSLV-II)  South Korea KARI 2,600 1,500 to SSO[82][83] 2[83] 2021 2022
OS-M1  China OneSpace 205[84] 143 to SSO 1 2019[85][p] 2019
Pegasus  United States Northrop Grumman 500[87] 44[87][88] 1990 2019
Proton-M / M+  Russia Khrunichev 21,600 (M)[89]
23,000 (M+)[90] 		6,150 (M)
6,920 (M+) 		108[91][92][93] 2001 2020
PSLV-CA  India ISRO 2,100[94] 1,100 to SSO 14[94] 2007 2019
PSLV-DL  India ISRO 1[94] 2019 2021
PSLV-QL  India ISRO 2[94] 2019 2019
PSLV-XL  India ISRO 3,800[94] 1,300 1,750 to SSO
550 to TMI[95] 		21[94] 2008 2020
Qased  Iran Revolutionary Guard Corps (IRGC) 2 2020 2022
Shavit  Israel IAI 300[96] 10[97] 1988 2020
Simorgh  Iran Iranian Space Agency 350[98] 2[98][q] 2017 2019
Soyuz-2.1a  Russia TsSKB-Progress 7,020 from Baikonur[99] 55[100][101][102] 2006[r] 2022
Soyuz-2.1b  Russia TsSKB-Progress 8,200 from Baikonur[99] 2,400[103] 62[101][104] 2006 2022
Soyuz-2-1v  Russia TsSKB-Progress 2,800[105] 1,400 to SSO 9[105] 2013 2022
SLS Block 1  United States NASA / Boeing
Northrop Grumman 		95,000[106] 27,000+ to TLI[107] 1 2022[108] 2022
SS-520  Japan IHI Aerospace 4[109] 2[110] 2017[111][s] 2018
SSLV  India ISRO 500[112] 300 to SSO 1[113] 2022 2022
Unha  North Korea KCST 100[114] 4[115] 2009[t] 2016
Vega  Europe ESA / ASI 1,500[u][116] 1,330 to SSO[117] 15[118] 2012 2020
Vega C  Europe ESA / ASI 2,200[u][119] 1[120] 2022 2022
  1. ^ Suborbital flight tests and on-pad explosions are excluded, but launches failing en route to orbit are included.
  2. ^ Reference altitude 500 km
  3. ^ for Starliner[10]
  4. ^ GTO payload is 5,550 kg when the first stage lands downrange on a drone ship (ASDS). Reduced to 3,500 kg if the first stage returns to the launch site (RTLS).[22]
  5. ^ Additionally, one rocket exploded on the launch pad in 2016.[26]
  6. ^ GTO payload is 8,000 kg when the core first-stage booster lands downrange on a drone ship (ASDS) and the side boosters return to the launch site (RTLS). Increased to 10,000 kg if all boosters land on drone ships.[22]
  7. ^ As of 2022, Falcon Heavy has only flown in partially reusable configuration; fully expendable configuration is considered operational in the sense that it is a simplified version of the reusable configuration.
  8. ^ GTO payload with enhanced engines, as of GSLV version 2A[37]
  9. ^ A suborbital test flight was conducted in 2014 (designated LVM-3/CARE) without the cryogenic upper stage (CUS).[40]
  10. ^ LVM3 M2 / OneWeb India-1 Mission.[41]
  11. ^ 5,100 kg to a 500-km Sun-synchronous orbit; 3,300 kg to 800 km[42]: 64–65 
  12. ^ A suborbital test flight was conducted in April 2018.[44]
  13. ^ A suborbital test flight was conducted in March 2012.[49]
  14. ^ Additionally, two suborbital missions were conducted in 2010 and 2011.[78]
  15. ^ Reference altitude 400 km
  16. ^ A suborbital test flight was conducted in May 2018.[86]
  17. ^ A suborbital test flight succeeded in 2016; both orbital flights in 2017 and 2019 failed.[98]
  18. ^ Suborbital test flight in 2004, without Fregat upper stage.[100]
  19. ^ A prior version of the SS-520 flew twice as a suborbital sounding rocket in 1998 and 2000. In 2017, the addition of a small third stage enabled orbital launches of ultra-light nano- or picosatellites.[109]
  20. ^ A suborbital test flight failed in 2006. The first two orbital missions failed in 2009 and 2012, and the rocket finally reached orbit in late 2012.[115]
  21. ^ a b Reference altitude 700 km

Upcoming rockets

Vehicle Origin Manufacturer Payload mass to ... (kg) Date of first flight
LEO GTO Other
Agnibaan  India AgniKul Cosmos 100 0 2022[citation needed]
Amur  Russia 10,500[121] 2026[121]
Antares 330  United States Northrop Grumman
Firefly Aerospace[a] 		> 8,000[122] TBA
Ariane 6 A62  Europe ArianeGroup 10,350[123]: 45  5,000[123]: 33  6,450 to SSO
3,000 to HEO
3,000 to TLI [123]: 40–49  		2023[124]
Ariane 6 A64  Europe ArianeGroup 21,650[123]: 46  11,500+ [123]: 33  14,900 to SSO
5,000 to GEO
8,400 to HEO
8,500 to TLI [123]: 40–49  		2023
Beta  United States
 Ukraine 		Firefly Aerospace 8,000[125] TBA 5,800 to SSO TBA
Bloostar  Spain Zero 2 Infinity 140[126] 75 to SSO[126] TBA
Blue Whale 1  South Korea Perigee Aerospace 63[127] 50 to SSO TBA
Cyclone-4M  Ukraine Yuzhnoye
Yuzhmash 		5,000[128] 1,000[129] 3,350 to SSO[128] 2023[130]
Chetak  India Bellatrix Aerospace 2023
DNLV  Malaysia Independence-X Aerospace 200 2023
Eris  Australia
 Singapore 		Gilmour Space Technologies 305[131] 2023[132]
H3  Japan Mitsubishi 4,000[133] 6,500[134] 4,000 to SSO[135] 2022[136]
Hyperbola-2  China i-Space 2,000[44] 2023[55]
Kuaizhou 21  China ExPace 20,000[137] 2025[51]
Long March 9  China CALT 150,000[138] 66,000[139] 53,000 to TLI[138]
40,000 to TMI[140] 		2030[141]
Miura 5  Spain PLD Space 900 450 to SSO 2024[142]
Neutron  United States
 New Zealand 		Rocket Lab 8,000 2024[143]
New Glenn  United States Blue Origin 45,000[144] 13,000 2023[145]
New Line 1
(partially reusable)[146] 		 China LinkSpace 200 to SSO[146] TBA
OS-M2  China OneSpace 390[84] 292 to SSO TBA
Qaem-100  Iran Islamic Revolutionary Guard Corps 80[147] TBA
Prime  United Kingdom Orbex 220[148] 150 to SSO[b][149] 2023[150]
Ravn X  United States Aevum 100[151] TBA
RFA One  Germany Rocket Factory Augsburg AG 1,600[152] 450[152] 2023[153]
RS1  United States ABL Space Systems 1,350[154] 400 1,000 to SSO
750 to MEO 		2022[155]
Skyrora XL  United States Skyrora 335[156] 315 to SSO[156] 2023[157]
Soyuz-5 / Irtysh  Russia TsSKB-Progress
RSC Energia 		18,000[158] 2,500 to GEO 2022[159][160]
SLS Block 1B[c]  United States NASA / Boeing
Northrop Grumman 		105,000[161] 37,000 to TLI[162] 2025[163]
SLS Block 2[d]  United States NASA / Boeing
Northrop Grumman 		130,000[164] 45,000 to HCO[162] late 2020s (TBD)
Spectrum  Germany Isar Aerospace 1,000[165] 700 to SSO[165] 2023[153]
Starship[166]
(Single launch) 		 United States SpaceX 100,000+[166][note 5] 21,000[167] 2022 (orbital)[168]
Starship[166]
(Additional refuelling launches) 		 United States SpaceX 100,000+[166][note 6] 100,000+
[166] 		100,000+ to Mars surface[166]
100,000+ to lunar surface[166] 		2023 (TBD)[168]
Terran 1  United States Relativity Space 1,250[169] 900 to SSO 2022[170]
Terran R  United States Relativity Space 20,000[169] 2024[169]
Vega E  Europe ESA / ASI 3,000[171] 2025[172]
Vikram 1[173]  India Skyroot Aerospace[174] 315 to 45º inclination 500 km LEO 200 to 500 km SSPO 2023[175]
Vikram 2[173]  India Skyroot Aerospace 520 to 45º inclination 500 km LEO 410 to 500 km SSPO TBA
Vikram 3[173]  India Skyroot Aerospace 720 to 45º inclination 500 km LEO 580 to 500 km SSPO TBA
Vulcan / Centaur  United States ULA 27,200[176] 14,400[176] 7,200 to GEO[176]
12,100 to TLI 		2023[177]
Yenisei[178]  Russia TsSKB-Progress
RSC Energia 		88,000 – 115,000[160] 27,000 to TLI[179][180][181] 2028[180]
Zero  Japan Interstellar Technologies 100 to SSO[b][182] 2023[183]
Zuljanah  Iran Iranian Space Agency 220[184] TBA
921 rocket  China CALT 25,000 to TLI[185] 2025[141]
Zhuque-2  China LandSpace 4,000[186] 2,000 to SSO 2022[55]
  1. ^ provides the first stage, including engines
  2. ^ a b Reference altitude 500 km
  3. ^ with EUS
  4. ^ with EUS and
    advanced boosters

Retired rockets

Vehicle Origin Manufacturer Mass to ... (kg) Launches
(+ suborbital) 		Date of flight
LEO GTO Other First Last
Antares 110–130  United States Orbital 5,100[5] 1,500 to SSO 5[5] 2013 2014
Ariane 1  Europe Aérospatiale 1,830[187] 11[187] 1979 1986
Ariane 2  Europe Aérospatiale 2,270[187] 6[187] 1986 1989
Ariane 3  Europe Aérospatiale 2,650[187] 11[187] 1984 1989
Ariane 4 40  Europe Aérospatiale 4,600[187] 2,105 2,740 to SSO 7[187] 1990 1999
Ariane 4 42L  Europe Aérospatiale 7,000[187] 3,480 4,500 to SSO 13[187] 1993 2002
Ariane 4 42P  Europe Aérospatiale 6,000[187] 2,930 3,400 to SSO 15[187] 1990 2002
Ariane 4 44L  Europe Aérospatiale 7,000[187] 4,720 6,000 to SSO 40[187] 1989 2003
Ariane 4 44LP  Europe Aérospatiale 7,000[187] 4,220 5,000 to SSO 26[187] 1988 2001
Ariane 4 44P  Europe Aérospatiale 6,500[187] 3,465 4,100 to SSO 15[187] 1991 2001
Ariane 5 G  Europe EADS Astrium 18,000[188] 6,900[188] 16[188] 1996 2003
Ariane 5 G+  Europe EADS Astrium 7,100[188] 3[188] 2004 2004
Ariane 5 GS  Europe EADS Astrium 16,000[189] 6,600[188] 6[188] 2005 2009[190]
Ariane 5 ES  Europe EADS Astrium 21,000[7] 8,000[188] 8[188] 2008 2018
ASLV  India ISRO[191] 150[192] 4[192] 1987 1994
Athena I  United States Lockheed Martin 795[193] 515 4[194] 1995 2001
Athena II  United States Lockheed Martin 1,800[195] 3[196] 1998 1999[197]
Atlas-Centaur  United States Lockheed 1,134[198] 2,222[199] 148 1962 1983
Atlas G  United States Lockheed 5,900[200] 2,222 1,179 to HCO[200] 7[200] 1984 1989
Atlas H/MSD  United States Lockheed 3,630[201] 5 1983 1987
Atlas I  United States Lockheed Martin 5,900[200] 2,340[200] 11[200] 1990 1997
Atlas II  United States Lockheed Martin 6,780[200] 2,810 2,000 to HCO[200] 10[200] 1991 1998
Atlas IIA  United States Lockheed Martin 7,316[200] 3,180 2,160 to HCO[200] 23[200] 1992 2002
Atlas IIAS  United States Lockheed Martin 8,618[200] 3,833 2,680 to HCO[200] 30[200] 1993 2004
Atlas IIIA  United States Lockheed Martin 8,686[200] 4,060 2,970 to HCO[200] 2[200] 2000 2004
Atlas IIIB/DEC  United States Lockheed Martin 10,759[200] 4,609[200] 1[200] 2002 2002
Atlas IIIB/SEC  United States Lockheed Martin 10,218[202] 4,193[200] 3[200] 2003 2005
Atlas V 401  United States ULA 9,050[9] 4,950 6,670 to SSO 41[9] 2002 2022
Atlas V 411  United States ULA 9,050[9] 6,075 8,495 to SSO 6[9] 2006 2020
Atlas V 421  United States ULA 9,050[9] 7,000 9,050 to SSO 9[9] 2007 2022
Atlas V 431  United States ULA 9,050[9] 7,800 9,050 to SSO 3[9] 2005 2016
Atlas V 501  United States ULA 8,250[9] 3,970 5,945 to SSO
1,500 to GEO 		7[9] 2010 2020
Atlas V 511  United States ULA 11,000[9] 5,250 7,820 to SSO
1,750 to GEO 		1[203] 2022 2022
Atlas V 521  United States ULA 13,300[9] 6,485 9,585 to SSO
2,760 to GEO 		2[9] 2003 2004
Atlas V 531  United States ULA 15,300[9] 7,425 11,160 to SSO
3,250 to GEO 		5[9] 2010 2022
Atlas V 541  United States ULA 17,100[9] 8,240 12,435 to SSO
3,730 to GEO 		9[9] 2011 2022
Black Arrow  United Kingdom RAE 73[204] 2 (+2) 1969[a] 1971
Commercial Titan III  United States Martin Marietta 13,100[205] 4 1990 1992
Delta 0300  United States McDonnell Douglas 340[206] 747 to SSO[207] 3[208] 1972 1973[209]
Delta 0900  United States McDonnell Douglas 1,300[210] 818 to SSO[208] 2[208] 1972 1972
Delta 1410  United States McDonnell Douglas 340[211] 1[208] 1975 1975
Delta 1604  United States McDonnell Douglas 390[212] 2[208] 1972 1973
Delta 1900  United States McDonnell Douglas 1,800[208] 1[208] 1973 1973
Delta 1910  United States McDonnell Douglas 1,066[213] 1[208] 1975 1975
Delta 1913  United States McDonnell Douglas 328[214] 1[208] 1973 1973
Delta 1914  United States McDonnell Douglas 680[215] 2[208] 1972 1973
Delta 2310  United States McDonnell Douglas 336[216] 3[208] 1974 1981
Delta 2313  United States McDonnell Douglas 243 to GEO[217] 3[208] 1974 1977
Delta 2910  United States McDonnell Douglas 1,887[208] 6[208] 1975 1978
Delta 2913  United States McDonnell Douglas 2,000[218] 700[218] 6[208] 1975 1976
Delta 2914  United States McDonnell Douglas 724[208] 30[208] 1974 1979
Delta 3910  United States McDonnell Douglas 2,494[208] 1,154 with PAM-D 10[208] 1980 1988
Delta 3913  United States McDonnell Douglas 816[219] 1[208] 1981 1981
Delta 3914  United States McDonnell Douglas 954[208] 13[208] 1975 1987
Delta 3920  United States McDonnell Douglas 3,452[208] 1,284 with PAM-D 10[208] 1982 1989
Delta 3924  United States McDonnell Douglas 1,104[208] 4[208] 1982 1984
Delta 4925  United States McDonnell Douglas 3,400[220] 1,312[208] 2[208] 1989 1990
Delta 5920  United States McDonnell Douglas 3,848[221] 1[208] 1989 1989
Delta II 6920  United States McDonnell Douglas 3,983[208] 3[208] 1990 1992
Delta II 6925  United States McDonnell Douglas 1,447[208] 14[208] 1989 1992
Delta II 7320  United States Boeing IDS / ULA 2,865[208] 1,651 to SSO 12[208] 1999 2015
Delta II 7326  United States Boeing IDS 934[208] 636 to TLI
629 to HCO 		3[208] 1998 2001
Delta II 7420  United States ULA 3,185[208] 1,966 to SSO 14[208] 1998 2018
Delta II 7425  United States Boeing IDS 1,100[208] 804 to HCO 4[208] 1998 2002
Delta II 7426  United States Boeing IDS 1,058[208] 734 to TLI
711 to HCO 		1[208] 1999 1999
Delta II 7920  United States Boeing IDS / ULA 5,030[208] 3,123 to SSO 29[208] 1998 2017
Delta II 7925  United States Boeing IDS / ULA 1,819[208] 1,177 to TLI
1,265 to HCO 		69[208] 1990 2009
Delta II-H 7920H  United States Boeing IDS / ULA 6,097[208] 3[208] 2003 2011
Delta II-H 7925H  United States Boeing IDS / ULA 2,171 1,508 to HCO[208] 3[208] 2003 2007
Delta III 8930  United States Boeing IDS 8,292[208] 3,810 3[208] 1998 2000
Delta IV M  United States Boeing IDS 9,440[13] 4,440 7,690 to polar 3[14] 2003 2006
Delta IV M+(4,2)  United States ULA 13,140[13] 6,390 10,250 to polar 14[14] 2002 2019
Delta IV M+(5,2)  United States ULA 11,470[13] 5,490 9,600 to polar 3[14] 2012 2018
Delta IV M+(5,4)  United States ULA 14,140[13] 7,300 11,600 to polar 8[14] 2009 2019
Diamant  France SEREB 107[222][223] 12 1965 1975
Dnepr  Ukraine Yuzhmash 3,700[224] 22[224] 1999 2015[225]
Energia[b]  Soviet Union NPO Energia 100,000[226] 20,000 to GEO[226]
32,000 to TLI[226] 		1 (failed to orbit)[227] 1987 1987
Energia-Buran  Soviet Union NPO Energia (Launcher)
NPO Molniya (Orbiter) 		30,000[226][c] 1 1988 1988
Falcon 1  United States SpaceX 470[228] 5[228] 2006 2009
Falcon 9 v1.0  United States SpaceX 10,450[229] 4,540[229] 5[230] 2010 2013
Falcon 9 v1.1  United States SpaceX 13,150[231][d] 4,850[231] 15[230] 2013 2016
Feng Bao 1  China Shanghai Bureau No.2 2,500[232] 8 (+3)[233] 1972 1981
GSLV Mk.I(a)  India ISRO 5,000[35] 1,540[234] 1[234] 2001 2001
GSLV Mk.I(b)  India ISRO 5,000[35] 2,150[234] 4[234] 2003 2007
GSLV Mk.I(c)  India ISRO 5,000[35] 1[234] 2010 2010
H-I  Japan
 United States 		Mitsubishi 1,400[235] 9 1986 1992
H-II / IIS  Japan Mitsubishi 10,060[236] 4,000[237] 7[237] 1994 1999
H-IIA 204  Japan Mitsubishi 5,950[42]: 48  5[43] 2006 2021
H-IIA 2022  Japan Mitsubishi 4,500[43] 3[43] 2005 2007
H-IIA 2024  Japan Mitsubishi 11,000[238] 5,000[43] 7[43] 2002 2008
H-IIB  Japan Mitsubishi 16,500 (ISS)[134] 8,000 8[239] 2009 2020
J-I  Japan Nissan Motors[240] 1,000[241] 0 (+1) 1996 1996
Kaituozhe-1  China CALT 100[242] 2 2002 2003
Kosmos-3M  Soviet Union
 Russia 		NPO Polyot 1,500[243] 442[244] 1967 2010
Lambda 4S  Japan Nissan Motors[240] 26[245] 5 1966 1970
Long March 1  China CALT 300[246] 2[247] 1970 1971
Long March 1D  China CALT 740[248] 0 (+3)[247] 1995[e] 2002
Long March 2A  China CALT 2,000[249] 4[58] 1974 1978
Long March 2E  China CALT 9,200[58] 7[58] 1990 1995
Long March 3  China CALT 5,000[60] 13[60] 1984 2000
Long March 3B  China CALT 11,200[59] 5,100 5,700 to SSO 12[60] 1996 2012
Long March 4A  China CALT 4,000 2[61] 1988 1990
M-V  Japan Nissan Motors[240] (1997–2000)
IHI Aerospace[17] (2000–2006) 		1,850[245] 7 1997 2006
Molniya  Soviet Union RSC Energia 1,800[250] 40[251] 1960 1967
Molniya-M  Soviet Union
 Russia 		RSC Energia 2,400[252] 280[253] 1965 2010
Mu-3C  Japan Nissan Motors[240] 195[245] 4 1974 1979
Mu-3H  Japan Nissan Motors[240] 300[245] 3 1977 1978
Mu-3S  Japan Nissan Motors[240] 300[245] 4 1980 1984
Mu-3SII  Japan Nissan Motors[240] 770[245] 8 1985 1995
Mu-4S  Japan Nissan Motors[240] 180[245] 4 1971 1972
N1  Soviet Union NPO Energia 95,000[254][255][256][f] 4[257] (never reached orbit) 1969 1972
N-I  Japan
 United States 		Mitsubishi 1,200[258] 7 1975 1982
N-II  Japan
 United States 		Mitsubishi 2,000[259] 8 1981 1987
Naro-1  South Korea
 Russia 		KARI/Khrunichev 100[260] 3 2009 2013
NOTS-EV-1 Pilot  United States United States Navy 1.05[261] 10 1958 1958
Paektusan  North Korea KCST 700[262] 0 (+1) 1998 1998
Polyot  Soviet Union RSC Energia 1,400 2 1963 1964
Proton-K  Soviet Union
 Russia 		Khrunichev 19,760[263] 4,930[264] 311[265] 1965 2012
PSLV-G  India ISRO 3,200[94] 1,050 1,600 to SSO 12[94] 1993 2016[266]
Rocket 3  United States Astra 100[267] 150 to SSO 7[268] 2020[267] 2022
Rokot  Russia Khrunichev 1,950[269] 1,200 to SSO 34[269] 1990 2019
Safir  Iran Iranian Space Agency 65[270] 7[270][g] 2008 2019
Saturn I  United States Chrysler (S-I)
Douglas (S-IV) 		9,000[271] 10[272] 1961 1965[272]
Saturn IB  United States Chrysler (S-IB)
Douglas (S-IVB) 		18,600[273] 9[274] 1966 1975
Saturn V  United States Boeing (S-IC)
North American (S-II)
Douglas (S-IVB) 		140,000[275][276] 47,000 to TLI[277] 13[278][279][h] 1967 1973
Scout  United States US Air Force/NASA 174[280] 125 1961 1994
Shtil'  Russia Makeyev 280–420[281] 2[282] 1998 2006
SLV  India ISRO 40[283] 4[283] 1979 1983[283]
Soyuz  Soviet Union RSC Energia 6,450 31[284] 1966 1976
Soyuz-FG  Russia TsSKB-Progress 6,900[285] 70[101][286] 2001 2019
Soyuz-L  Soviet Union RSC Energia 5,500 3[287] 1970 1971
Soyuz-M  Soviet Union RSC Energia 6,600 8[288] 1971 1976
Soyuz ST-A  Russia
 Europe 		TsSKB-Progress
Arianespace 		7,800 from Kourou[289] 2,810 with Fregat[290] 9[101] 2011 2021
Soyuz ST-B  Russia
 Europe 		TsSKB-Progress
Arianespace 		9,000 from Kourou[291] 3,250 with Fregat[290] 4,400 to SSO[292] 18[101] 2011 2022
Soyuz-U  Soviet Union
 Russia 		TsSKB-Progress 6,650 from Baikonour[293]
6,150 from Plesetsk[293] 		786[101][102][294] 1973 2017
Soyuz-U2  Soviet Union
 Russia 		TsSKB-Progress 7,050 72[295] 1982 1995
Space Shuttle  United States ATK (SRBs)
Martin Marietta (External tank)
Rockwell (Orbiter) 		24,400[c]
3,550 to escape with IUS[296] 135[298] 1981 2011
Sputnik 8K71PS  Soviet Union RSC Energia 500[299] 2 1957 1957
Sputnik 8A91  Soviet Union RSC Energia 1,327 2 1958 1958
Start-1  Russia MITT 532 350 to SSO[300] 5[301] 1993 2006
Strela  Russia Khrunichev 1,400[302] 3[303] 2003 2014
Titan II GLV  United States Martin Marietta 3,600[304] 11 (+1) 1964 1966
Titan II(23)G  United States Martin Marietta 3,600[305] 13 1988 2003
Titan IIIA  United States Martin Marietta 3,100[306] 4 1964 1965
Titan IIIB  United States Martin Marietta 3,000[307] 70 1966 1987
Titan IIIC  United States Martin Marietta 13,100[308] 36 1965 1982
Titan IIID  United States Martin Marietta 12,300[309] 22 1971 1982
Titan IIIE  United States Martin Marietta 15,400[310] 7 1974 1977
Titan 34D  United States Martin Marietta 4,515[311] 15 1982 1989
Titan IVA  United States Martin Marietta 17,110[312] 4,944 with IUS
22[313] 1989 1998
Titan IVB  United States Lockheed Martin 21,682[314] 5,761[314]
(9,000 with upper stage) 		17[313] 1997 2005
Tsyklon-2A  Soviet Union Yuzhmash 3,350[315] 8[316] 1967 1969
Tsyklon-2  Soviet Union
 Ukraine 		Yuzhmash 2,820[317] 106[318] 1969 2006[318]
Tsyklon-3  Soviet Union
 Ukraine 		Yuzhmash 1,920[319] 122[320] 1977 2009[320]
Vanguard  United States Martin 9[321] 11 (+1) 1957 1959
VLS-1  Brazil AEB, IAE 380[322] 2[i] (never reached orbit) 1997 2003
Volna  Russia Makeyev 100[323] 1 (+5)[282] 1995[j] 2005[282]
Voskhod  Soviet Union RSC Energia 6,000[324] 306 1963 1976
Vostok-L  Soviet Union RSC Energia 390 to TLI[325] 4 1960 1960
Vostok-K  Soviet Union RSC Energia 2,460[326] 16 1960 1964
Vostok-2  Soviet Union RSC Energia 4,730[326] 45 1962 1967
Vostok-2M  Soviet Union RSC Energia 1,300[327] 93 1964 1991
Soyuz/Vostok  Soviet Union RSC Energia 6,000[328] 2 1965 1966
Zenit-2  Soviet Union
 Ukraine 		Yuzhnoye 13,740[329] 36[330] 1985 2004[331]
Zenit-2M / 2SLB  Ukraine Yuzhnoye 13,920[329] 2[330] 2007 2011
Zenit-3F  Ukraine Yuzhnoye 1,740 to GEO[332] 4[333] 2011 2017
Zenit-3SL  Ukraine Yuzhmash
RSC Energia 		7,000[333] 6,160 36[333] 1999 2014
Zenit-3SLB / 3M  Ukraine Yuzhmash
RSC Energia 		3,750[333] 6[333] 2008 2013
Zhuque-1  China LandSpace 300[334] 200 to SSO 1[335] 2018[335] 2018
  1. ^ First suborbital test in 1969, first orbital launch attempt in 1970
  2. ^ Without Buran, and assuming payload providing orbital insertion
  3. ^ a b The U.S. Space Shuttle Transportation System and the Soviet Energia-Buran system consist of launch vehicle rockets and returnable spaceplane orbiter. Payload values listed here are for the mass of the payload in cargo bay of the spaceplanes, excluding the mass of the spaceplanes themselves.
  4. ^ The SpaceX website lists the F9 payload to LEO as 13,150kg. The payload to GTO is listed as 4,850kg. However, SpaceX has stated that these numbers include a 30% margin to accommodate re-usability.
  5. ^ Suborbital test flights in 1995, 1997 and 2002, no orbital launches attempted
  6. ^ The N1 rocket was initially designed for 75 t LEO capacity and launch attempts were made with this version, but there were studies to increase the payload capacity to 90–95 t, if a liquid-hydrogen upper stage engine could be developed.
  7. ^ Additionally, two rockets exploded on the launch pad, one in 2012 and one in 2019.[270]
  8. ^ The Saturn V made 13 launches, 12 of which reached the correct orbits, and the other (Apollo 6) reached a different orbit than the one which had been planned; however, some mission objectives could still be completed; NASA, Saturn V News Reference, Appendix: Saturn V Flight History (1968) Archived 2011-05-17 at the Wayback Machine. For more information, see the Saturn V article. The Saturn V launch record is usually quoted as having never failed, e.g. "The rocket was masterminded by Wernher Von Braun and did not fail in any of its flights", Alan Lawrie and Robert Godwin; Saturn, but the Apollo 6 launch should be considered a partial mission failure. The 13th launch of Saturn V was in special configuration (SA-513) with the Skylab.
  9. ^ A third rocket exploded before launch.
  10. ^ First orbital launch attempt in 2005

Launch systems by country

The following chart shows the number of launch systems developed in each country, and broken down by operational status. Rocket variants are not distinguished; i.e., the Atlas V series is only counted once for all its configurations 401–431, 501–551, 552, and N22.

10
20
30
40
50
AUS
BRZ
CHN
EUR
ESP
FRA
IND
IRN
ISR
JPN
NKR
NZL
RUS
SKR
TWN
UKR
UK
USA
  •   Operational
  •   In development
  •   Retired

See also

Notes

  1. ^ There are many different methods. Each method has drawbacks and advantages, and spacecraft propulsion is an active area of research. However, most spacecraft today are propelled by forcing a gas from the back/rear of the vehicle at very high speed through a supersonic de Laval nozzle. This sort of engine is called a rocket engine.
  2. ^ The first medieval rockets were solid-fuel rockets powered by gunpowder; they were used by the Chinese, Indians, Mongols and Arabs, in warfare as early as the 13th century.
  3. ^ Such as the Pegasus rocket and SpaceShipOne.
  4. ^ Most satellites have simple reliable chemical thrusters (often monopropellant rockets) or resistojet rockets for orbital station-keeping and some use momentum wheels for attitude control. Soviet bloc satellites have used electric propulsion for decades, and newer Western geo-orbiting spacecraft are starting to use them for north-south stationkeeping and orbit raising. Interplanetary vehicles mostly use chemical rockets as well, although a few have used ion thrusters and Hall effect thrusters (two different types of electric propulsion) to great success.
  5. ^ Elon Musk [@elonmusk] (31 March 2020). "Mass of initial SN ships will be a little high & Isp a little low, but, over time, it will be ~150t to LEO fully reusable" (Tweet) – via Twitter.
  6. ^ Elon Musk [@elonmusk] (31 March 2020). "Mass of initial SN ships will be a little high & Isp a little low, but, over time, it will be ~150t to LEO fully reusable" (Tweet) – via Twitter.

References

  1. ^ "Firefly Alpha". Firefly Aerospace. Retrieved 29 October 2019.
  2. ^ a b c "Angara Launch Vehicle Family". Khrunichev State Research and Production Space Center. Retrieved 2 September 2018.
  3. ^ Krebs, Gunter. "Angara Family". Gunter's Space Page. Retrieved 31 December 2021.
  4. ^ Mooney, Justin (2022-04-30). "Russia launches first orbital Angara 1.2 rocket with military payload". NASASpaceFlight.com. Retrieved 2022-08-12.
  5. ^ a b c Krebs, Gunter. "Antares (Taurus-2)". Gunter's Space Page. Retrieved 1 December 2019.
  6. ^ Krebs, Gunter. "Antares 230". Gunter's Space Page. Retrieved 20 November 2019.
  7. ^ a b "Ariane 5 Users Manual" (PDF). Issue 4. Arianespace. p. 39 (ISS orbit). Archived from the original (PDF) on 27 September 2007. Retrieved 13 November 2007.
  8. ^ "Ariane 5 sets new record on latest launch". ESA. 24 October 2021. Retrieved 25 October 2021.
  9. ^ a b c d e f g h i j k l m n o p q r s Krebs, Gunter. "Atlas-5". Gunter's Space Page. Retrieved 29 July 2022.
  10. ^ Egan, Barbara [@barbegan13] (October 15, 2016). "We are calling the config N22. No payload fairing with the Starliner on board" (Tweet) – via Twitter.
  11. ^ Roulette, Joey (22 December 2019). "'Bull's-eye' landing in New Mexico for Boeing's Starliner astronaut capsule". Reuters. Retrieved 22 December 2019.
  12. ^ Krebs, Gunter. "Ceres-1". Gunter's Space Page. Retrieved 6 February 2022.
  13. ^ a b c d e "Delta IV Launch Services User's Guide, June 2013" (PDF). United Launch Alliance. June 2013. pp. 2–10. Retrieved 9 October 2017.
  14. ^ a b c d e Krebs, Gunter. "Delta-4". Gunter's Space Page. Retrieved 17 March 2019.
  15. ^ a b "Rocket Lab Increases Electron Payload Capacity, Enabling Interplanetary Missions and Reusability". Rocket Lab. Retrieved 2020-08-04.
  16. ^ "Completed Missions". Rocket Lab. Retrieved 2022-03-09.
  17. ^ a b "Projects&Products". IHI Aerospace. Archived from the original on 6 April 2011. Retrieved 8 March 2011.
  18. ^ "Epsilon a solid propellant launch vehicle for new age" (PDF). IHI Aerospace. Retrieved 3 February 2018.
  19. ^ Krebs, Gunter. "Epsilon". Gunter's Space Page. Retrieved 18 January 2019.
  20. ^ Mogg, Trevor (May 24, 2019). "SpaceX joins internet-from-space race with launch of 60 Starlink satellites". www.digitaltrends.com.
  21. ^ a b c d "Capabilities & Services". SpaceX. Retrieved 5 April 2017.
  22. ^ a b Koenigsmann, Hans (3 October 2018). SpaceX performance tiers to GTO. IAC 2018. Retrieved 23 October 2018.
  23. ^ de Selding, Peter B. (June 15, 2016). "Iridium's SpaceX launch slowed by Vandenberg bottleneck". SpaceNews. Retrieved June 21, 2016.
  24. ^ Krebs, Gunter. "Falcon-9 v1.2 (Falcon-9FT)". Gunter's Space Page. Retrieved 19 November 2018.
  25. ^ Krebs, Gunter. "Falcon-9 v1.2 (Block 5) (Falcon-9FT (Block 5))". Gunter's Space Page. Retrieved 20 November 2019.
  26. ^ Malik, Tariq (1 September 2016). "Launchpad Explosion Destroys SpaceX Falcon 9 Rocket, Satellite in Florida". Space.com. Retrieved 1 September 2016.
  27. ^ Krebs, Gunter. "Falcon-9 v1.2(ex) (Falcon-9FT(ex))". Gunter's Space Page. Retrieved 29 June 2018.
  28. ^ Krebs, Gunter. "Falcon-9 v1.2 (Block 5)(ex) (Falcon-9FT (Block 5)(ex))". Gunter's Space Page. Retrieved 10 August 2019.
  29. ^ Either 2 or 3 boosters recoverable
  30. ^ Musk, Elon. Making Life Multiplanetary. SpaceX. Event occurs at 15:35. Archived from the original on 2021-12-12. Retrieved 22 March 2018 – via YouTube. BFR in fully reusable configuration, without any orbital refueling, we expect to have a payload capability of 150 tonnes to low Earth orbit and that compares to about 30 for Falcon Heavy
  31. ^ Elon Musk [@elonmusk] (12 February 2018). "Side boosters landing on droneships & center expended is only ~10% performance penalty vs fully expended. Cost is only slightly higher than an expended F9, so around $95M" (Tweet) – via Twitter.
  32. ^ Krebs, Gunter. "Falcon-Heavy". Gunter's Space Page. Retrieved 15 April 2019.
  33. ^ Krebs, Gunter. "Falcon-Heavy (Block 5)". Gunter's Space Page. Retrieved 15 July 2019.
  34. ^ a b c "SpaceX". SpaceX. Retrieved 2020-08-29.
  35. ^ a b c d "Geosynchronous Satellite Launch Vehicle (GSLV)". ISRO. Retrieved August 31, 2018.
  36. ^ Subramanian, T.S. (14 September 2018). "ISRO developing vehicle to launch small satellites". Frontline. Retrieved 29 August 2018.
  37. ^ a b Krebs, Gunter. "GSLV". Gunter's Space Page. Retrieved 19 December 2018.
  38. ^ "GSLV MkIII-M1 Successfully Launches Chandrayaan-2 spacecraft - ISRO". www.isro.gov.in. Retrieved 2019-12-01.
  39. ^ Krebs, Gunter. "GSLV Mk.3 (LVM-3)". Gunter's Space Page. Retrieved 10 August 2019.
  40. ^ "Crew module Atmospheric Re-entry Experiment (CARE)". ISRO. 18 December 2014. Retrieved 4 September 2018.
  41. ^ "LVM3 M2 / OneWeb India-1 Mission". ISRO. 23 October 2022. Retrieved 23 October 2022.
  42. ^ a b c d e "H-IIA – User's Manual" (PDF). 4.0. Mitsubishi Heavy Industries, MHI Launch Services. February 2015. YET04001. Retrieved 4 September 2018.
  43. ^ a b c d e f Krebs, Gunter. "H-2A". Gunter's Space Page. Retrieved 12 November 2018.
  44. ^ a b c Jones, Andrew (15 May 2018). "Chinese commercial launch sector nears takeoff with suborbital rocket test". SpaceNews. Retrieved 16 August 2018.
  45. ^ "Chinese rocket company suffers third consecutive launch failure". SpaceNews. 2022-05-13. Retrieved 2022-05-13.
  46. ^ Huang, Echo (25 July 2019). "A private Chinese space firm successfully launched a rocket into orbit". Quartz. Retrieved 10 August 2019.
  47. ^ a b Krebs, Gunter. "Jielong-1 (Smart Dragon-1, SD 1)". Gunter's Space Page. Retrieved 2 November 2019.
  48. ^ a b Krebs, Gunter. "Kaituozhe-2 (KT-2)". Gunter's Space Page. Retrieved 2 November 2019.
  49. ^ a b c Krebs, Gunter. "Kuaizhou-1 (KZ-1) / Fei Tian 1". Gunter's Space Page. Retrieved 8 January 2020.
  50. ^ "快舟十一号小型固体运载火箭(KZ-11)：推迟到2018年首飞" [Kuaizhou 11 small solid launch vehicle (KZ-11): First flight planned for 2018] (in Chinese). October 30, 2017. Retrieved March 10, 2018.
  51. ^ a b "Kuai Zhou (Fast Vessel)". China Space Report. Archived from the original on March 11, 2018. Retrieved March 10, 2018.
  52. ^ Clark, Stephen (August 31, 2018). "Virgin Orbit nears first test flights with air-launched rocket". Spaceflight Now. Retrieved September 1, 2018.
  53. ^ "LauncherOne service guide" (PDF). Virgin Orbit. 2017. Archived from the original (PDF) on 2018-03-28. Retrieved 2017-08-07.
  54. ^ "产品信息 - 中科宇航". www.cas-space.com. Retrieved 2022-08-13.
  55. ^ a b c Jones, Andrew (6 July 2022). "New launch vehicles set for test flights from China's Jiuquan spaceport". SpaceNews. Retrieved 8 July 2022.
  56. ^ Krebs, Gunter. "Zhongke-1 (ZK-1, Lijian-1)". Gunter's Space Page. Retrieved 31 July 2021.
  57. ^ "Two satellites with secretive missions launched by China". Spaceflight Now. 12 October 2018. Retrieved 12 October 2018.
  58. ^ a b c d e f Krebs, Gunter. "CZ-2 (Chang Zheng-2)". Gunter's Space Page. Retrieved 5 October 2021.
  59. ^ a b c d "LM-3A Series Launch Vehicles User's Manual Issue 2011" (PDF). 2011. Archived from the original (PDF) on 17 July 2015. Retrieved 17 August 2015.
  60. ^ a b c d e f Krebs, Gunter. "CZ-3 (Chang Zheng-3)". Gunter's Space Page. Retrieved 5 October 2021.
  61. ^ a b c d Krebs, Gunter. "CZ-4 (Chang Zheng-4)". Gunter's Space Page. Retrieved 5 October 2021.
  62. ^ Krebs, Gunter. "CZ-4C (Chang Zheng-4C)". Gunter's Space Page. Retrieved 16 August 2018.
  63. ^ a b c Qin, Xudong; Long, Lehao; Rong, Yi (April 2016). "我国航天运输系统成就与展望" [Achievements and prospects of China's space transportation system]. 深空探测学报 (Journal of Deep Space Exploration) (in Chinese). 3 (4): 315–322. doi:10.15982/j.issn.2095-7777.2016.04.003. Retrieved 28 August 2017.
  64. ^ a b c d Krebs, Gunter. "CZ-5 (Chang Zheng-5)". Gunter's Space Page. Retrieved 24 August 2021.
  65. ^ a b Jones, Andrew (14 February 2020). "China prepares to launch new rockets as part of push to boost space program". space.com. Retrieved 14 February 2020.
  66. ^ Barbosa, Rui (19 September 2015). "China conducts debut launch of Long March 6". NASASpaceFlight.com. Retrieved 2015-09-26.
  67. ^ a b Krebs, Gunter. "CZ-6 (Chang Zheng-6)". Gunter's Space Page. Retrieved 5 October 2021.
  68. ^ "China conducts debut launch of Long March 6". Xinhua Net. 29 March 2022. Retrieved 2022-04-14.
  69. ^ ""长征七号"运载火箭具备近地轨道13.5吨、700千米太阳同步轨道5.5吨运载能力". 新华网. 2011-12-29. Archived from the original on 2015-11-02.
  70. ^ a b Krebs, Gunter. "CZ-7 (Chang Zheng-7)". Gunter's Space Page. Retrieved 5 October 2021.
  71. ^ "长征七号首飞成功 空间实验室任务大幕拉开" [Successful maiden flight of the Long March 7 mission Damulakai]. www.spacechina.com (in Chinese). 2016-06-25. Archived from the original on 28 June 2016. Retrieved 25 June 2016.
  72. ^ Krebs, Gunter. "CZ-8 (Chang Zheng-8)". Gunter's Space Page. Retrieved 5 October 2021.
  73. ^ Chan, Kai Yee (8 October 2015). "China reveals CZ-11 anti-ASAT rocket". Chinese Daily Mail. Retrieved 4 September 2018.
  74. ^ Krebs, Gunter. "CZ-11 (Chang Zheng-11)". Gunter's Space Page. Retrieved 5 October 2021.
  75. ^ "Minotaur I Space Launch Vehicle—Fact Sheet" (PDF). Orbital Sciences Corporation. 2012. Retrieved 28 February 2012. Spacecraft mass-to-orbit of up to 580 kg to LEO (28.5 deg, 185 km)
  76. ^ Krebs, Gunter. "Minotaur-1 (OSP-SLV)". Gunter's Space Page. Retrieved 5 October 2021.
  77. ^ "Minotaur IV – Fact sheet" (PDF). Orbital Sciences Corporation. 2010. BR06005d. Archived from the original (PDF) on 8 October 2010. Retrieved 4 March 2009.
  78. ^ a b c d Krebs, Gunter. "Minotaur-3/-4/-5/-6 (OSP-2 Peacekeeper SLV)". Gunter's Space Page. Retrieved 5 October 2021.
  79. ^ "Taurus". Orbital Sciences Corporation. 2012. Archived from the original on 22 July 2012.
  80. ^ "Minotaur-C, Ground-Launched Space Launch Vehicle" (PDF). Orbital Sciences Corporation. 2014. FS003_02_2998. Archived from the original (PDF) on 14 July 2014.
  81. ^ Krebs, Gunter. "Taurus / Minotaur-C". Gunter's Space Page. Retrieved 30 November 2017.
  82. ^ "Korea Space Launch Vehicle (Nuri)". Korea Aerospace Research Institute. Retrieved 1 December 2019.
  83. ^ a b "South Korea's KSLV-II conducts maiden launch". NASASpaceFlight.com. 2021-10-21. Retrieved 2021-10-22.
  84. ^ a b Goh, Deyana (5 July 2018). "Chinese startup One Space successfully tests first stage engine for orbital rocket". Spacetech Asia. Retrieved 16 August 2018.
  85. ^ Krebs, Gunter. "OS-M (Chongqing SQX)". Gunter's Space Page. Retrieved 15 April 2019.
  86. ^ Jones, Andrew (17 May 2018). "Chinese company OneSpace sends OS-X rocket to 40 km in maiden flight". GBTimes. Retrieved 17 May 2018.
  87. ^ a b Krebs, Gunter. "Pegasus". Gunter's Space Page. Retrieved 11 October 2019.
  88. ^ Clark, Stephen (11 October 2019). "NASA Awards Launch for Orbital's Pegasus Rocket". Spaceflight Now. Retrieved 11 October 2019.
  89. ^ "Proton Launch System Mission Planner's Guide, LKEB-9812-1990" (PDF). International Launch Services. p. 2. Archived from the original on 27 October 2007. Retrieved 12 November 2007. LEO i = 51.6°, H = 200 km circular ... GTO (1800 m/s from GSO) i = 31.0°, Hp = 2100 km, Ha = 35,786 km
  90. ^ "Proton Launch System Mission Planner's Guide Section 2 LV Performance" (PDF). International Launch Services. Retrieved 2016-04-07.
  91. ^ Krebs, Gunter. "Proton-M Blok-DM-2". Gunter's Space Page. Retrieved 9 October 2017.
  92. ^ Krebs, Gunter. "Proton-M Blok-DM-03". Gunter's Space Page. Retrieved 10 August 2019.
  93. ^ Krebs, Gunter. "Proton-K and -M Briz-M". Gunter's Space Page. Retrieved 12 October 2019.
  94. ^ a b c d e f g h Krebs, Gunter. "PSLV". Gunter's Space Page. Retrieved 1 December 2019.
  95. ^ Arunan, S.; Satish, R. (25 September 2015). "Mars Orbiter Mission spacecraft and its challenges". Current Science. 109 (6): 1061–1069. doi:10.18520/v109/i6/1061-1069.
  96. ^ "Shavit". Space Launch Report. 13 September 2016. Retrieved 4 September 2018. LEO Payload 200 x 1,600 km x 143 deg – Shavit: 160 kg – Shavit-1: 225 kg – Shavit-2: 300 kg
  97. ^ Krebs, Gunter. "Shavit". Gunter's Space Pages. Retrieved 20 December 2016.
  98. ^ a b c Krebs, Gunter. "Simorgh (Safir-2)". Gunter's Space Page. Retrieved 15 January 2019.
  99. ^ a b "Soyuz-2.1 Launch Vehicle". Progress Rocket Space Centre. Retrieved 2 February 2018.
  100. ^ a b Krebs, Gunter. "Soyuz-2-1a (14A14)". Gunter's Space Page. Retrieved 10 August 2019.
  101. ^ a b c d e f Krebs, Gunter. "Soyuz with Fregat upper stage". Gunter's Space Page. Retrieved 26 September 2019.
  102. ^ a b Krebs, Gunter. "Soyuz with Ikar and Volga upper stages". Gunter's Space Page. Retrieved 20 December 2016.
  103. ^ "Soyuz Rocket". Space Launch Report. Retrieved 17 May 2015.
  104. ^ Krebs, Gunter. "Soyuz-2-1b". Gunter's Space Page. Retrieved 27 September 2019.
  105. ^ a b Krebs, Gunter. "Soyuz core only". Gunter's Space Page. Retrieved 10 August 2019.
  106. ^ Harbaugh, Jennifer (9 July 2018). "The Great Escape: SLS Provides Power for Missions to the Moon". NASA. Archived from the original on 11 December 2019. Retrieved 16 November 2022. Public Domain This article incorporates text from this source, which is in the public domain.
  107. ^ [1] (PDF). 20 August 2018. Archived (PDF) from the original on 7 August 2020. Retrieved 16 November 2022. Public Domain This article incorporates text from this source, which is in the public domain.
  108. ^ https://www.theguardian.com/science/live/2022/nov/16/artemis-1-nasa-rocket-launch-moon-mission-space-live-updates
  109. ^ a b Krebs, Gunter. "SS-520". Gunter's Space Page. Retrieved 5 November 2017.
  110. ^ Graham, William (3 February 2018). "Japanese sounding rocket claims record-breaking orbital launch". NASASpaceFlight. Retrieved 3 February 2018.
  111. ^ "Experimental Launch of World's Smallest Orbital Space Rocket ends in Failure". Spaceflight 101. 14 January 2017. Retrieved 5 November 2017.
  112. ^ Krebs, Gunter. "SSLV". Gunter's Space Page. Retrieved 16 August 2018.
  113. ^ "India's new SSLV rocket fails in first launch". SpaceNews. 2022-08-07. Retrieved 2022-08-14.
  114. ^ "Kwangmyongsong 3, 3-2 (KMS 3, 3-2)".
  115. ^ a b Krebs, Gunter. "Unha ("Taepodong-2")". Gunter's Space Page. Retrieved 20 December 2016.
  116. ^ "Vega overview". Arianespace. Retrieved 7 June 2018.
  117. ^ "Vega User's Manual" (PDF). Issue 4. Arianespace. April 2014. pp. 2–10. Retrieved 4 September 2018.
  118. ^ Krebs, Gunter. "Vega". Gunter's Space Page. Retrieved 15 July 2019.
  119. ^ "Vega C: Launcher". Avio. Retrieved 7 June 2018.
  120. ^ "Vega C lifts off on maiden flight". SpaceNews. 2022-07-13. Retrieved 2022-08-12.
  121. ^ a b Berger, Eric (7 October 2020). "Russian space corporation unveils planned "Amur" rocket—and it looks familiar". Ars Technica. Retrieved 7 October 2020.
  122. ^ "Northrop Grumman Teams with Firefly Aerospace to Develop Antares Rocket Upgrade and New Medium Launch Vehicle". Northrop Grumman Newsroom. Retrieved 2022-08-08.
  123. ^ a b c d e f Lagier, Roland (March 2018). "Ariane 6 User's Manual Issue 1 Revision 0" (PDF). Arianespace. Retrieved 27 May 2018.
  124. ^ "Ariane 6 launch debut pushed into 2023". SpaceNews. 2022-06-13. Retrieved 2022-06-14.
  125. ^ "Firefly Beta". Firefly Aerospace. Retrieved 18 January 2021.
  126. ^ a b "Bloostar Launch Vehicle Payload User's Guide" (PDF). Revision 2. Zero 2 Infinity. January 2018. Z2I-BS-TN-1-0316-R2. Retrieved 4 September 2018.
  127. ^ "Perigee Aerospace Inc". Retrieved 2020-06-14.
  128. ^ a b Boucher, Marc (14 March 2017). "Exclusive: Maritime Launch Services Selects Nova Scotia Site for Spaceport Over 13 Other Locations". SpaceQ. Retrieved 18 March 2017.
  129. ^ Krebs, Gunter. "Tsiklon-4M (Cyclone-4M)". Gunter's Space Page. Retrieved 11 April 2017.
  130. ^ Willick, Frances (12 May 2021). "Canso spaceport secures $10.5M, aims for first launch next year". CBC News. Retrieved 14 May 2021.
  131. ^ "LAUNCH". Gilmour Space. Retrieved 2021-05-29.
  132. ^ "Gilmour Space announces first 'Caravan' rideshare mission to LEO". Gilmour Space Technologies (Press release). 19 September 2022. Retrieved 19 September 2022. [The company] is expecting to launch its first Eris vehicle from the Bowen Orbital Spaceport in Queensland, Australia, early next year.
  133. ^ Only the X00 version of the H3 is intended for LEO launches.[failed verification] The higher capability X02 and X03 variants could presumably launch significantly more payload to LEO, but are not specified for this mission. Space Launch Report: H3 Data Sheet, retrieved 20 Feb. 2019/
  134. ^ a b "MHI Launch Services: Launch Vehicles". Mitsubishi Heavy Industries, MHI Launch Services. Retrieved 4 September 2018.
  135. ^ 新型基幹ロケットの開発状況について [Development status of the new carrier rocket] (PDF) (in Japanese). JAXA. 2 July 2015. p. 3. Retrieved July 8, 2015.
  136. ^ Kanayama, Lee (6 September 2021). "Japan's H3 rocket awaiting final engine certification for first flight". NASASpaceFlight. Retrieved 6 October 2021.
  137. ^ "China to test large solid-fuel rocket engine". China Daily. December 25, 2017. Retrieved March 10, 2018.
  138. ^ a b Jones, Andrew (28 June 2021). "China's super heavy rocket to construct space-based solar power station". Retrieved 8 January 2022.
  139. ^ "China to develop new series of carrier rockets: expert". Xinhua.net. 2 July 2018. Archived from the original on July 2, 2018. Retrieved 25 September 2018.
  140. ^ Jones, Andrew (5 July 2018). "China reveals details for super-heavy-lift Long March 9 and reusable Long March 8 rockets". SpaceNews. Retrieved 4 September 2018.
  141. ^ a b Berger, Eric (24 February 2021). "China officially plans to move ahead with super-heavy Long March 9 rocket". Ars Technica. Retrieved 1 March 2021.
  142. ^ "PLD Space, la ambición de lanzar satélites con cohetes reutilizables" [PLD Space, and the ambition to launch satellites with reusable rockets]. El País (in Spanish). 11 August 2020. Retrieved 17 August 2020.
  143. ^ "JP Introducing Neutron". YouTube. 2021-03-01. Archived from the original on 2021-12-12. Retrieved 2021-03-01.
  144. ^ Foust, Jeff (8 March 2017). "Eutelsat first customer for Blue Origin's New Glenn". SpaceNews. Retrieved 8 March 2017.
  145. ^ Foust, Jeff (23 March 2022). "Vulcan Centaur on schedule for first launch in 2022 as New Glenn slips". SpaceNews. Retrieved 24 March 2022.
  146. ^ a b Lin, Jeffrey; Singer, P.W. (18 December 2017). "China could become a major space power by 2050". Popular Science. Retrieved 4 September 2018.
  147. ^ "IRGC Launches Satellite Carrier into Space - Politics news". Tasnim News Agency. Retrieved 2022-11-07.
  148. ^ "About us". Orbex. Retrieved 4 September 2018. Orbex can accommodate a range of payload capacities between 100kg-220kg, to altitudes of between 200km-1250km.
  149. ^ Foust, Jeff (18 July 2018). "Orbex stakes claim to European smallsat launch market". SpaceNews. Retrieved 4 September 2018.
  150. ^ Foust, Jeff (2022-10-18). "Orbex raises Series C round". SpaceNews. Retrieved 2022-10-19.
  151. ^ Berger, Eric (2020-12-03). "Meet Ravn X—a fully autonomous, air-launched rocket for small satellites". Ars Technica. Retrieved 2020-12-04.
  152. ^ a b "LAUNCHER – Rocket Factory Augsburg". Retrieved 2021-09-18.
  153. ^ a b "German Launch Providers Isar Aerospace and RFA Eye Maiden Launches in 2023 – Parabolic Arc". Retrieved 2022-08-13.
  154. ^ "ABL Space Systems".
  155. ^ "ABL Space Systems to launch Project Kuiper's first satellites in 2022". SpaceNews. 2021-11-01. Retrieved 2022-01-02.
  156. ^ a b "Skyrora XL Rocket | Skyrora". www.skyrora.com. Retrieved 2022-08-19.
  157. ^ "Second stage static fire engine test moves Skyrora closer to UK launch | SKYRORA". www.skyrora.com. Retrieved 2022-08-19.
  158. ^ Zak, Anatoly (7 August 2017). "Preliminary design for Soyuz-5 races to completion". Russian Space Web. Retrieved 2 September 2018.
  159. ^ Zak, Anatoly (13 November 2017). "Russia's "new" next manned rocket detailed". Russian Space Web. Retrieved 2 September 2018.
  160. ^ a b "Russia to launch super-heavy rocket to Moon in 2032–2035". TASS. 23 January 2018. Retrieved 6 June 2018.
  161. ^ "Space Launch System" (PDF). NASA Facts. NASA. 11 October 2017. FS-2017-09-92-MSFC. Retrieved 4 September 2018.
  162. ^ a b Harbaugh, Jennifer (9 July 2018). "The Great Escape: SLS Provides Power for Missions to the Moon". NASA. Retrieved 4 September 2018.
  163. ^ "Forward to the Moon: NASA's Strategic Plan for Human Exploration" (PDF). NASA. 4 September 2019.
  164. ^ Creech, Stephen (April 2014). "NASA's Space Launch System: A Capability for Deep Space Exploration" (PDF). NASA. p. 2. Retrieved 4 September 2018.
  165. ^ a b "Spectrum". Isar Aerospace. Retrieved 2022-03-05.
  166. ^ a b c d e f g "Starship". SpaceX. Archived from the original on 30 September 2019. Retrieved 1 October 2019.
  167. ^ "Starship Users Guide" (PDF). spacex.com. Retrieved 1 April 2020.
  168. ^ a b "FAA delays completion of Starship environmental review". SpaceNews. 2021-12-28. Retrieved 2022-01-02.
  169. ^ a b c "Terran". Relativity Space. Retrieved 3 February 2022.
  170. ^ "Relativity is pushing back the demo launch of its Terran 1 rocket to early 2022". TechCrunch. Retrieved 2022-01-02.
  171. ^ "Vega E: M10 motor / Mira". Avio. Archived from the original on 19 April 2019. Retrieved 7 June 2018.
  172. ^ Henry, Caleb (7 November 2019). "Avio anticipating Vega C upgrade funding at ESA ministerial, Vega return to flight in March". SpaceNews. Retrieved 17 August 2020.
  173. ^ a b c "Launch Vehicle". Skyroot Aerospace. 2019-01-10. Retrieved 2019-04-21.
  174. ^ "Skyroot Aerospace". Skyroot Aerospace. Retrieved 2019-04-21.
  175. ^ "Skyroot Aerospace's Mission Prarambh: A closer look at India's first private rocket launch". Moneycontrol. Retrieved 2022-11-11.
  176. ^ a b c "Rocket Rundown – A Fleet Overview" (PDF). ULA. November 2019. Retrieved April 14, 2020.
  177. ^ "ULA Sets Path Forward for Inaugural Vulcan Flight Test". www.ulalaunch.com. Retrieved 2022-10-14.
  178. ^ Zak, Anatoly (19 February 2019). "The Yenisei super-heavy rocket". RussianSpaceWeb. Retrieved 20 February 2019.
  179. ^ Zak, Anatoly (24 November 2017). "Russia charts new roadmap to super-heavy rocket". Russian Space Web. Retrieved 6 June 2018.
  180. ^ a b Zak, Anatoly (8 February 2019). "Russia Is Now Working on a Super Heavy Rocket of Its Own". Popular Mechanics. Retrieved 20 February 2019.
  181. ^ "Roscosmos unveils characteristics of super-heavy rockets for flights to the Moon (In Russian)". RIA NOVOSTI. 24 April 2019.
  182. ^ Werner, Debra (9 August 2018). "Japan's Interstellar Technologies goes full throttle toward small orbital rocket". SpaceNews. Retrieved 11 August 2018.
  183. ^ Yamanaka, Hirofumi; Kugai, Shoko (27 May 2020). "LNG-powered rocket offers boost to Japan's private space industry". Nikkei Asia. Retrieved 30 April 2021.
  184. ^ Axe, David. "Iran's New Space Rocket Could Double As A Nuclear Missile". Forbes. Retrieved 2021-03-08.
  185. ^ Jones, Andrew (1 October 2020). "China is building a new rocket to fly its astronauts on the moon". Space.com. Retrieved 1 March 2021.
  186. ^ Jones, Andrew (10 July 2018). "Commercial Chinese companies set sights on methalox rockets, first orbital launches". SpaceNews. Retrieved 16 August 2018.
  187. ^ a b c d e f g h i j k l m n o p q r Krebs, Gunter. "Ariane-1, -2, -3, -4". Gunter's Space Page. Retrieved 2 August 2011.
  188. ^ a b c d e f g h i Krebs, Gunter. "Ariane-5". Gunter's Space Page. Retrieved 31 December 2021.
  189. ^ "Ariane 5". andegraf.com. Retrieved April 27, 2018.
  190. ^ "Final launch of Ariane 5 GS completes busy year / Launchers / Our Activities / ESA". European Space Agency. 2009-12-19. Retrieved 2013-11-04.
  191. ^ "Welcome To ISRO :: Launch Vehicles". ISRO. Retrieved 2013-11-04.
  192. ^ a b Krebs, Gunter. "SLV-3 / ASLV". Gunter's Space Page. Retrieved 18 December 2016.
  193. ^ "Athena-1 (LLV-1 / LMLV-1)".
  194. ^ "Athena-1". Astronautix.com. Archived from the original on 2013-10-20. Retrieved 2013-11-04.
  195. ^ NASA, Athena Mission Planner’s Guide 26 August 2012
  196. ^ "Athena-2". Astronautix.com. Archived from the original on 2013-11-08. Retrieved 2013-11-04.
  197. ^ "Athena-2 (LLV-2 / LMLV-2)".
  198. ^ "Atlas Centaur LV-3C Development".
  199. ^ "Atlas Centaur".
  200. ^ a b c d e f g h i j k l m n o p q r s t u v w Krebs, Gunter. "Atlas Centaur". Gunter's Space Page. Retrieved 1 August 2011.
  201. ^ astronautix.com, Atlas H
  202. ^ astronautix.com, Atlas IIIB Archived 2002-05-01 at the Wayback Machine
  203. ^ "ULA launches two space surveillance satellites for U.S. Space Force". SpaceNews. 2022-01-21. Retrieved 2022-01-24.
  204. ^ Encyclopedia Astronautica, Black Arrow Archived 2007-12-06 at the Wayback Machine
  205. ^ astronautix.com, Titan III Archived 2014-12-25 at the Wayback Machine
  206. ^ "WMO OSCAR – Satellite: NOAA-3".
  207. ^ "NASA – NSSDCA – Spacecraft – Details".
  208. ^ a b c d e f g h i j k l m n o p q r s t u v w x y z aa ab ac ad ae af ag ah ai aj ak al am an ao ap aq ar as at au av aw ax ay az ba Krebs, Gunter. "Delta". Gunter's Space Page. Retrieved 16 September 2018.
  209. ^ Wade, Mark. "Delta 0300". Encyclopedia Astronautica. Archived from the original on 11 October 2011. Retrieved 2 August 2011.
  210. ^ Wade, Mark. "Delta 0900". Encyclopedia Astronautica. Archived from the original on 11 October 2011. Retrieved 2 August 2011.
  211. ^ "GEOS 3".
  212. ^ "1972 – 2616 – Flight Archive".
  213. ^ "OSO 8".
  214. ^ "Explorer: RAE B".
  215. ^ "Delta-1914".
  216. ^ "NASA – NSSDCA – Spacecraft – Details".
  217. ^ "Skynet 2A, 2B".
  218. ^ a b Wade, Mark. "Delta 2913". Encyclopedia Astronautica. Archived from the original on 11 October 2011. Retrieved 2 August 2011.
  219. ^ "Explorer: DE 1, 2".
  220. ^ Wade, Mark. "Delta 4000". Encyclopedia Astronautica. Archived from the original on 11 October 2011. Retrieved 2 August 2011.
  221. ^ Wade, Mark. "Delta 5000". Encyclopedia Astronautica. Archived from the original on 11 October 2011. Retrieved 2 August 2011.
  222. ^ "Aura / Signe 3 (D 2B)".
  223. ^ Space Skyrocket, Diamant, retrieved 19 December 2015
  224. ^ a b Krebs, Gunter. "Dnepr". Gunter's Space Page. Retrieved 18 December 2016.
  225. ^ Clark, Stephen (30 December 2016). "Iridium satellites closed up for launch on Falcon 9 rocket". Spaceflight Now. Retrieved 30 December 2016. Russian officials have said they plan to discontinue Dnepr launches.
  226. ^ a b c d "S.P.Korolev RSC Energia – LAUNCHERS". Energia. Archived from the original on 2016-03-03. Retrieved 2010-08-01.
  227. ^ Wade, Mark. "Energia". Encyclopedia Astronautica. Archived from the original on 11 October 2011. Retrieved 9 August 2010.
  228. ^ a b Krebs, Gunter. "Falcon-1". Gunter's Space Page. Retrieved 18 December 2016.
  229. ^ a b "Falcon 9 Overview". SpaceX. 2011. Archived from the original on 2012-01-18. Retrieved 2011-12-01.
  230. ^ a b Krebs, Gunter. "Falcon-9". Gunter's Space Page. Retrieved 24 May 2018.
  231. ^ a b "Falcon 9". SpaceX. 2012-11-16. Archived from the original on 5 August 2014.
  232. ^ Feng Bao 1, part of CZ family
  233. ^ Krebs, Gunter. "FB-1 (Feng Bao-1)". Gunter's Space Page. Retrieved 17 August 2018.
  234. ^ a b c d e Krebs, Gunter. "GSLV". Gunter's Space Page. Retrieved 18 December 2016.
  235. ^ "JERS (Fuyo)".
  236. ^ astronautix.com, H-2 Archived 2008-07-06 at the Wayback Machine
  237. ^ a b Krebs, Gunter. "H-2". Gunter's Space Page. Retrieved 1 August 2011.
  238. ^ astronautix.com H-IIA 2024 Archived 2011-10-11 at the Wayback Machine
  239. ^ Krebs, Gunter. "H-2B". Gunter's Space Page. Retrieved 24 September 2019.
  240. ^ a b c d e f g h "Nissan Heritage Collection online【その他】プリンス自動車工業小史". Nissan Motors. Retrieved 8 March 2011.
  241. ^ "JAXA – J-I Launch Vehicle".
  242. ^ astronautix.com Kaituozhe-1, also called KY-1 Archived 2008-05-12 at the Wayback Machine
  243. ^ "Cosmos-1, 3, 3M and 3MU – SL-8 – C-1".
  244. ^ "Kosmos-3M (11K65M)". Archived from the original on 2013-06-02. Retrieved 2015-12-21.
  245. ^ a b c d e f g "Satellite Launch Vehicles". Institute of Space and Astronautical Science (ISAS). Retrieved 4 March 2011.
  246. ^ astronautix.com, Long March 1, also called CZ-1
  247. ^ a b Krebs, Gunter. "CZ-1 (Chang Zheng-1)". Gunter's Space Page. Retrieved 12 February 2014.
  248. ^ astronautix.com, Long March 1D (CZ-1D) Archived 2002-05-25 at the Wayback Machine
  249. ^ astronautix.com Long March 2A – CZ-2A Archived 2008-05-16 at the Wayback Machine
  250. ^ astronautix.com, Encyclopedia Astronautica, Molniya 8K78M Archived 2012-05-08 at the Wayback Machine
  251. ^ Krebs, Gunter. "Molniya (8K78)". Gunter's Space Page. Retrieved 18 December 2016.
  252. ^ "US-K (73D6)".
  253. ^ Krebs, Gunter. "Molniya and Soyuz with upper stages". Gunter's Space Page. Retrieved 18 December 2016.
  254. ^ "Complex N1-L3". Energia.ru. Retrieved 2013-11-04.
  255. ^ "L3". Astronautix.com. Archived from the original on 2012-12-01. Retrieved 2013-11-04.
  256. ^ "RSC "Energia" – History". Energia.ru. 2011-04-12. Retrieved 2013-11-04.
  257. ^ Wade, Mark. "N1". Encyclopedia Astronautica. Archived from the original on June 12, 2002. Retrieved 9 August 2010.
  258. ^ astronautix.com, N-I- Delta Archived 2008-07-24 at the Wayback Machine
  259. ^ astronautix.com, Encyclopedia Astronautica, N-2 Archived 2013-11-08 at the Wayback Machine
  260. ^ "STSAT 2C".
  261. ^ LePage, Andrew J. (July 1998). "NOTSNIK: The Navy's Secret Satellite Program". Spaceviews. Archived from the original on May 21, 2003. Retrieved 2009-01-17.
  262. ^ Korea, By Christoph Bluth,
  263. ^ Encyclopedia Astronautica, Proton-K
  264. ^ "Launch Vehicles".
  265. ^ "Proton". Astronautix.com. Archived from the original on September 13, 2008. Retrieved 2013-11-04.
  266. ^ "Outcome Budget 2016–2017" (PDF). Government of India, Department of Space. 2016. Retrieved 15 September 2018. Currently, two versions of PSLV are operational, namely PSLV-XL (with six extended version of Strap-on motors) and the PSLV Core-alone (without Strap-on motors).
  267. ^ a b Vance, Ashlee (3 February 2020). "A Small-Rocket Maker Is Running a Different Kind of Space Race". Bloomberg News. Retrieved 3 February 2020.
  268. ^ "Astra cancels Rocket 3 to focus on larger vehicle". SpaceNews. 2022-08-05. Retrieved 2022-08-12.
  269. ^ a b Krebs, Gunter. "Rokot (Rockot)". Gunter's Space Page. Retrieved 31 August 2019.
  270. ^ a b c Krebs, Gunter. "Safir". Gunter's Space Pages. Retrieved 2 March 2019.
  271. ^ astronautix.com, Saturn I Archived 2010-12-07 at the Wayback Machine
  272. ^ a b "Saturn-1 & Saturn-1B". Space.skyrocket.de. Retrieved 2013-11-04.
  273. ^ Encyclopedia Astronautica, Saturn IB Archived 2011-05-14 at the Wayback Machine
  274. ^ Bilstein, Roger E. "Appendix C: Saturn Family/Mission Data". Stages to Saturn A Technological History of the Apollo/Saturn Launch Vehicles. NASA History Office. Retrieved 7 April 2011.
  275. ^ Alternatives for Future U.S. Space-Launch Capabilities (PDF), The Congress of the United States. Congressional Budget Office, October 2006, pp. X, 1, 4, 9
  276. ^ Thomas P. Stafford (1991), America at the Threshold – Report of the Synthesis Group on America's Space Exploration Initiative, p. 31
  277. ^ "Rocket and Space Technology". Braeunig.us. Retrieved 2013-11-04.
  278. ^ Alan Lawrie and Robert Godwin, Saturn, 2005 (paperback, Apogee Books Space Series, 2010), ISBN 1-894959-19-1
  279. ^ John Duncan, Saturn V Flight History Archived 2011-08-05 at the Wayback Machine (1999), web page (accessed 20 August 2010)
  280. ^ "NASA – Scout Launch Vehicle Program".
  281. ^ "Vysota / Volna / Shtil".
  282. ^ a b c "Vysota / Volna / Shtil". Retrieved 2014-12-23.
  283. ^ a b c "SLV-3". Retrieved 13 February 2014.
  284. ^ Krebs, Gunter. "Soyuz (11A511)". Gunter's Space Page. Retrieved 20 December 2016.
  285. ^ "Soyuz-FG Launch Vehicle". Progress Rocket Space Centre. Retrieved 16 May 2015.
  286. ^ Krebs, Gunter. "Soyuz-FG (11A511U-FG)". Gunter's Space Page. Retrieved 25 September 2019.
  287. ^ Krebs, Gunter. "Soyuz-L (11A511L)". Gunter's Space Page. Retrieved 20 December 2016.
  288. ^ Krebs, Gunter. "Soyuz-M (11A511M)". Gunter's Space Page. Retrieved 20 December 2016.
  289. ^ "Soyuz-ST". Encyclopedia Astronautica. Archived from the original on 24 August 2015. Retrieved 17 May 2015.
  290. ^ a b "Soyuz-ST Launch Vehicle". Progress Rocket Space Centre. Retrieved 17 May 2015.
  291. ^ "Soyuz 2 Launch Vehicle". Russian Space Web. Retrieved 19 May 2015.
  292. ^ "Soyuz overview". Arianespace. Retrieved 7 June 2018.
  293. ^ a b "Soyuz-U Launch Vehicle". JSC "RCC" Progress. Retrieved 16 May 2015.
  294. ^ Krebs, Gunter. "Soyuz-U (11A511U)". Gunter's Space Page. Retrieved 20 December 2016.
  295. ^ Krebs, Gunter. "Soyuz-U2 (11A511U2)". Gunter's Space Page. Retrieved 20 December 2016.
  296. ^ a b Krebs, Gunter. "Shuttle (STS)". Gunter's Space Page. Retrieved 14 July 2014.
  297. ^ "SPACE TRANSPORTATION SYSTEM PAYLOADS". Kennedy Space Center. 2000. Retrieved 14 July 2014.
  298. ^ "NASA – Space Shuttle". NASA. Retrieved 2012-07-25.
  299. ^ "Sputnik 2 (PS-2 #1)".
  300. ^ "EROS B".
  301. ^ "Start-1".
  302. ^ "Strela launcher".
  303. ^ "Strela". Gunter's Space Page. Retrieved 23 Dec 2014.
  304. ^ astronautix.com, Titan II GLV Archived 2016-02-28 at the Wayback Machine
  305. ^ astronautix.com, Titan 23G Archived 2016-03-04 at the Wayback Machine
  306. ^ Encyclopedia Astronautica, Titan 3A Archived 2008-03-07 at the Wayback Machine
  307. ^ Encyclopedia Astronautica, Titan 3B Archived 2012-10-25 at the Wayback Machine
  308. ^ astronautix.com, Titan IIIC Archived 2014-12-25 at the Wayback Machine
  309. ^ astronautix.com, Titan IIID Archived 2016-03-04 at the Wayback Machine
  310. ^ astronautix.com, Titan IIIE Archived 2015-12-02 at the Wayback Machine
  311. ^ astronautix.com, Titan 34D Archived 2008-06-30 at the Wayback Machine
  312. ^ a b "Titan-4". Gunter's Space Page. Retrieved 14 July 2014.
  313. ^ a b "Titan-4". Space.skyrocket.de. Retrieved 2013-11-04.
  314. ^ a b "Fact Sheet – Titan IVB". United States Air Force. Retrieved 2007-11-12.[permanent dead link]
  315. ^ astronautix.com, Tsyklon-2A Archived 2013-05-22 at the Wayback Machine
  316. ^ "Tsiklon-2A (11K67)". Space.skyrocket.de. Retrieved 2013-11-04.
  317. ^ astronautix.com, Tsyklon-2 Archived 2013-05-22 at the Wayback Machine
  318. ^ a b "Tsiklon-2 (11K69)". Space.skyrocket.de. Retrieved 2013-11-04.
  319. ^ nasaspaceflight.com, Tsyklon-3
  320. ^ a b "Tsiklon-3 (11K68)". Space.skyrocket.de. Retrieved 2013-11-04.
  321. ^ astronautix.com, vanguard Archived 2002-05-06 at the Wayback Machine
  322. ^ "VLS".
  323. ^ "IRDT 1, 2, 2R".
  324. ^ Handbook of Space Engineering, Archaeology, and Heritage by Ann Darrin, Beth L. O'Leary, page 116
  325. ^ "NASA – NSSDCA – Spacecraft – Details".
  326. ^ a b "Spacecraft – Vostok".
  327. ^ "Meteor-2 (11F632)".
  328. ^ astronautix.com, Soyuz/Vostok Archived 2010-01-07 at the Wayback Machine
  329. ^ a b Ed Kyle. "Zenit Data Sheet". Spacelaunchreport.com. Retrieved 2013-11-04.
  330. ^ a b Krebs, Gunter. "Zenit-2". Gunter's Space Pages. Retrieved 20 December 2016.
  331. ^ "Zenit launch vehicle". Russianspaceweb.com. Retrieved 2013-11-04.
  332. ^ "Elektro-L 1, 2, 3".
  333. ^ a b c d e Krebs, Gunter. "Zenit-3". Gunter's Space Page. Retrieved 28 December 2017.
  334. ^ Jones, Andrew (2 August 2018). "Landspace of China to launch first rocket in Q4 2018". SpaceNews. Retrieved 16 August 2018.
  335. ^ a b Barbosa, Rui C. (27 October 2018). "Chinese commercial provider LandSpace launches Weilai-1 on a Zhuque-1 rockets – fails to make orbit". NASASpaceFlight.com. Retrieved 27 October 2018.
Wikimedia Commons has media related to Rocket comparisons.
Retrieved from "https://en.wikipedia.org/w/index.php?title=Comparison_of_orbital_launch_systems&oldid=1124950139"