Wikipedia

Comparison of retired orbital launch systems

Retired rockets edit

Vehicle Origin Manufacturer Height Mass to ... (kg) Reuse Launches

(+ suborbital)

Launch Site (s) Date of flight
LEO GTO Other First Last
Antares 110–130   United States Orbital 40.5-41.9 m 5,100[1] 1,500 to SSO No 5[1] 2013 2014
Antares 230 / 230+   United States Northrop Grumman 42.5 m 8,200[1] 3,000 to SSO[a] No 13 2016 2023
Ariane 1   Europe Aérospatiale 49.1 m 1,830[2] No 11[2] 1979 1986
Ariane 2   Europe Aérospatiale 49.1 m 2,270[2] No 6[2] 1986 1989
Ariane 3   Europe Aérospatiale 49.1 m 2,650[2] No 11[2] 1984 1989
Ariane 4 40   Europe Aérospatiale 58.7 m 4,600[2] 2,105 2,740 to SSO No 7[2] 1990 1999
Ariane 4 42L   Europe Aérospatiale 58.7 m 7,000[2] 3,480 4,500 to SSO No 13[2] 1993 2002
Ariane 4 42P   Europe Aérospatiale 58.7 m 6,000[2] 2,930 3,400 to SSO No 15[2] 1990 2002
Ariane 4 44L   Europe Aérospatiale 58.7 m 7,000[2] 4,720 6,000 to SSO No 40[2] 1989 2003
Ariane 4 44LP   Europe Aérospatiale 58.7 m 7,000[2] 4,220 5,000 to SSO No 26[2] 1988 2001
Ariane 4 44P   Europe Aérospatiale 58.7 m 6,500[2] 3,465 4,100 to SSO No 15[2] 1991 2001
Ariane 5 G   Europe EADS Astrium 47.5 m 18,000[3] 6,900[3] No 16[3] 1996 2003
Ariane 5 G+   Europe EADS Astrium 48 m 7,100[3] No 3[3] 2004 2004
Ariane 5 GS   Europe EADS Astrium 48 m 16,000[4] 6,600[3] No 6[3] 2005 2009[5]
Ariane 5 ES   Europe EADS Astrium 50.7 m 21,000[6] 8,000[3] No 8[3] 2008 2018
Ariane 5 ECA   Europe EADS Astrium 52.6 m 21,000[6] 11,210[7] No 84 2002 2023
ASLV   India ISRO[8] 23.5 m 150[9] No 4[9] 1987 1994
Athena I LLV-1   United States Lockheed Martin 18.4 m 500 No 1 1995 1995
Athena I   United States Lockheed Martin 18.9 m 795[10] 515 No 3 1997 2001
Athena II   United States Lockheed Martin 28.2 m 1,800[11] No 3[12] 1998 1999[13]
Black Arrow   United Kingdom RAE 13 m 73[14] No 2 (+2) 1969[b] 1971
Blue Scout II   United States Vought 24 m 30 No 3 1961 1961
Ceres-1 (1)[c]   China Galactic Energy 18.5 m 350 No 1 2020 2020
Ceres-1 (2)[c]   China Galactic Energy 19.5 m 400 No 1 2021 2021
Commercial Titan III   United States Martin Marietta 47.3 m 13,100[16] No 4 1990 1992
Conestoga 1620   United States Space Services 15.2 m 1179 No 1 1995 1995
Diamant A   France SEREB 18.9 m 80 No 4 1965 1967
Diamant B   France SEREB 23.5 m 115 No 5 1970 1973
Diamant BP4   France SEREB 21.6 m 153 No 3 1975 1975
Dnepr   Ukraine Yuzhmash 34.3 m 3,700[17] No 22[17] 1999 2015[18]
Energia[d]   Soviet Union NPO Energia 58.8 m 105,000 20,000 to GEO[19]

32,000 to TLI[19]

No 1 (failed to orbit) 1987 1987
Energia-Buran   Soviet Union NPO Energia

NPO Molniya

58.8 m 30,000[19][e] Yes 1 1988 1988
Epsilon   Japan IHI[20] 24.4 m 1,200 N/A 450 to SSO No 1 2013 2022
Epsilon (enhanced)   Japan IHI[20] 26 m 1,500[21] N/A 590 to SSO[21] No 6[21]
Europa I   Europe ELDO 31.7 m 1,440 200 No 3 1968 1970
Europa II   Europe ELDO 31.7 m 360 No 1 1971 1971
Falcon 1   United States SpaceX 21 m 470[22] No 5[22] 2006 2009
Falcon 9 v1.0   United States SpaceX 47.8 m 9,000 3,400 No 5 2010 2013
Falcon 9 v1.1   United States SpaceX 68.4 m 13,150[23][f] 4,850[23] No 15[24] 2013 2016
Falcon 9 Full Thrust   United States SpaceX 70 m 17,400[25] 5,500[25] 9,600 to polar[26] Yes 36 2015 2018
22,800[25] 8,300[25] No
Feng Bao 1   China Shanghai Bureau No.2 33 m 2,500[27] No 8 (+3)[28] 1972 1981
GSLV Mk.I(a)   India ISRO 49.1 m 5,000[29] 1,540[30] No 1[30] 2001 2001
GSLV Mk.I(b)   India ISRO 49.1 m 5,000[29] 2,150[30] No 4[30] 2003 2007
GSLV Mk.I(c)   India ISRO 49.1 m 5,000[29] No 1[30] 2010 2010
H-I   Japan

  United States

Mitsubishi 42 m 1,400[31] No 9 1986 1992
H-II / IIS   Japan Mitsubishi 49 m 10,060[32] 4,000[33] No 7[33] 1994 1999
H-IIA 204   Japan Mitsubishi 53 m 15,000 5,950[34]: 48  No 5[35] 2006 2021
H-IIA 2022   Japan Mitsubishi 53 m 4,500[35] No 3[35] 2005 2007
H-IIA 2024   Japan Mitsubishi 57 m 11,000[36] 5,000[35] No 7[35] 2002 2008
H-IIB   Japan Mitsubishi 56.6 m 16,500 (ISS)[37] 8,000 No 8[38] 2009 2020
Hyperbola-1 (1)[g]   China i-Space 20.9 m 260 No 1 2019 2019
Juno I   United States Chrysler 21.2 m 11 No 1 1958 1959
Juno II   United States Chrysler 24 m 41 6 to TLI No 10 1958 1961
Kaituozhe-1   China CALT 13.6 m 40 No 2 2002 2003
Kaituozhe-2   China CASC 16.8 m 800[40] No 1[40] 2017 2017
Kosmos   Soviet Union NPO Polyot 29.6 m 350 No 38 1961 1967
Kosmos-1   Soviet Union NPO Polyot 26.3 m 1,400 No 8 1964 1965
Kosmos-2   Soviet Union NPO Polyot 31 m 300 No 127 1965 1977
Kosmos-3   Soviet Union NPO Polyot 32.4 m 1,400 No 6 1966 1968
Kosmos-3M   Soviet Union

  Russia

NPO Polyot 32.4 m 1,500[41] No 445 1967 2010
Kosmos-3MRB   Soviet Union NPO Polyot 32.4 m 1,500 No 10 1980 1988
Lambda 4S   Japan Nissan Motors[42] 16.5 m 26[43] No 5 1966 1970
LauncherOne   United States Virgin Orbit 21.3 m 500 300 to SSO No 6 2020 2023
Long March 1   China CALT 29.9 m 300[44] No 2[45] 1970 1971
Long March 1D   China CALT 28.2 m 740[46] No 0 (+3)[45] 1995[h] 2002
Long March 2A   China CALT 32 m 2,000[47] No 4[48] 1974 1978
Long March 2E   China CALT 49.7 m 9,200[48] No 7[48] 1990 1995
Long March 3   China CALT 43.3 m 5,000[49] No 13[49] 1984 2000
Long March 3B   China CALT 54.8 m 11,200[50] 5,100 5,700 to SSO No 12[49] 1996 2012
Long March 4A   China CALT 41.9 m 4,000 No 2[51] 1988 1990
M-V   Japan Nissan Motors[42] (1997–2000)

IHI Aerospace[20] (2000–2006)

30.8 m 1,850[43] No 7 1997 2006
Molniya   Soviet Union RSC Energia 43.4 m 1,800[52] No 40[53] 1960 1967
Molniya-M   Soviet Union

  Russia

RSC Energia 43.4 m 2,400[54] No 280[55] 1965 2010
Mu-4S   Japan Nissan Motors[42] 23.6 m 180[43] No 4 1971 1972
Mu-3C   Japan Nissan Motors[42] 20.2 m 195[43] No 4 1974 1979
Mu-3H   Japan Nissan Motors[42] 23.8 m 300[43] No 3 1977 1978
Mu-3S   Japan Nissan Motors[42] 23.8 m 300[43] No 4 1980 1984
Mu-3SII   Japan Nissan Motors[42] 27.8 m 770[43] No 8 1985 1995
N1   Soviet Union NPO Energia 105.3 m 95,000[i] No 4 1969 1972
N-I   Japan

  United States

Mitsubishi 34 m 1,200[56] No 7 1975 1982
N-II   Japan

  United States

Mitsubishi 35 m 2,000[57] No 8 1981 1987
Naro-1   South Korea

  Russia

KARI Khrunichev 33 m 100[58] No 3 2009 2013
OS-M1   China OneSpace 19 m 205[59] 143 to SSO No 1 2019[60][j] 2019
Paektusan-1   North Korea KCST 25.8 m 20 No 1 1998 1998
Pegasus   United States Northrop Grumman 15.4 m 455 No 6 1990 1994
Pegasus H   United States Northrop Grumman 15.4 m 544 No 4 1995 2000
Pilot II   United States United States Navy 4.4 m N/A 1.05 to MEO No 10 1958 1958
Polyot   Soviet Union RSC Energia 30 m 1,400 No 2 1963 1964
Proton (UR-500)   Soviet Union Khrunichev 39.8 m 12,200 No 4 1965 1966
Proton-K   Soviet Union

  Russia

Khrunichev 50 m 19,760[62] 4,930[63] No 311[64] 1965 2012
PSLV-G   India ISRO 44 m 3,200[65] 1,050 1,600 to SSO No 12[65] 1993 2016[66]
Rocket 3.0   United States Astra 11.6 m 100 No 1 2020 2020
Rocket 3.1   United States Astra 11.6 m 100 No 1 2020 2020
Rocket 3.2   United States Astra 11.6 m 100 No 1 2020 2020
Rocket 3.3   United States Astra 13.1 m 100[67] 150 to SSO No 5 2021 2022
Rokot-K   Russia Khrunichev 25.5 m No 4 1990 1999
Rokot-KM   Russia Khrunichev 29.1 m 1,950[68] 1,200 to SSO No 31 2000 2019
RS1 B1   United States ABL Space Systems 27 m 1,350[69] 400 975 to SSO

750 to MEO

No 1 2023[70] 2023
Safir-1   Iran Iranian Space Agency 22.6 m 27 No 2 2008 2009
Safir-1A   Iran Iranian Space Agency 22.6 m 15 No 1 2011 2011
Safir-1B   Iran Iranian Space Agency 22.6 m 50 No 1 2012 2012
Safir-1B+   Iran Iranian Space Agency 22.6 m 52 No 5 2012 2019
Saturn I   United States Chrysler (S-I)

Douglas (S-IV)

50-57.4 m 9,000[71] No 10[72] 1961 1965[72]
Saturn IB   United States Chrysler (S-IB)

Douglas (S-IVB)

56.1-68.1 m 18,600[73] No 9[74] 1966 1975
Saturn V   United States Boeing (S-IC)

North American (S-II) Douglas (S-IVB)

110.6 m 140,000[75][76] 47,000 to TLI No 13[k] 1967 1973
Scout X-1   United States Vought 21.8 m 59 No 4 1960 1961
Scout X-2   United States Vought 21.8 m 76 No 1 1962 1962
Scout X-2M   United States Vought 21.8 m 76 No 3 1962 1963
Scout X-2B   United States Vought 21.8 m 76 No 1 1963 1963
Scout X-3   United States Vought 21.8 m 87 No 5 1962 1964
Scout X-3M   United States Vought 21.8 m 87 No 1 1963 1963
Scout X-4   United States Vought 22.8 m 103 No 11 1963 1965
Scout A   United States NASA 22.8 m 110 No 11 1965 1970
Scout A-1   United States NASA 22.8 m 122 No 1 1973 1973
Scout B   United States NASA 22.8 m 110 No 20 1965 1971
Scout B-1   United States NASA 22.8 m 143 No 5 1971 1976
Scout D-1   United States NASA 22.9 m 182 No 14 1972 1979
Scout E-1   United States NASA 22.8 m 193 No 1 1974 1974
Scout F-1   United States NASA 22.9 m 192 No 2 1975 1975
Scout G-1   United States NASA 22.9 m 208 No 18 1979 1994
Shavit   Israel IAI 17.7 m 160 No 2 1988 1990
Shavit-1   Israel IAI 19.7 m 225 No 4 1995 2004
Shtil-1   Russia Makeyev 14.8 m 280–420[77] No 2[78] 1998 2006
SLV-3   India ISRO 22 m 40[79] No 4[79] 1979 1983[79]
Soyuz   Soviet Union RSC Energia 45.6 m 6,450 No 31[80] 1966 1976
Soyuz-FG   Russia TsSKB-Progress 49.5 m 6,900[81] No 70[82][83] 2001 2019
Soyuz-L   Soviet Union RSC Energia 50 m 5,500 No 3[84] 1970 1971
Soyuz-M   Soviet Union RSC Energia 50 m 6,600 No 8[85] 1971 1976
Soyuz ST-A   Russia

  Europe

TsSKB-Progress

Arianespace

46.3 m 7,800 from Kourou[86] 2,810 with Fregat[87] No 9[82] 2011 2021
Soyuz ST-B   Russia

  Europe

TsSKB-Progress

Arianespace

46.3 m 9,000 from Kourou[88] 3,250 with Fregat[87] 4,400 to SSO[89] No 18[82] 2011 2022
Soyuz-U   Soviet Union

  Russia

TsSKB-Progress 51.1 m 6,650 from Baikonour[90]

6,150 from Plesetsk[90]

No 786[82][91][92] 1973 2017
Soyuz-U2   Soviet Union

  Russia

TsSKB-Progress 34.5 m 7,050 No 72[93] 1982 1995
Space Shuttle   United States ATK (SRBs)

Martin Marietta (External tank) Rockwell (Orbiter)

56.1 m 24,400[e]
3,550 to escape with IUS Yes 135[96] 1981 2011
SPARK   United States UHAerojet RocketdyneSandia 17 m 300 No 1 2015 2015
Sparta   United States ABMA/Chrysler 21.8 m 45 No 10 1966 1967
Sputnik 8K71PS   Soviet Union RSC Energia 30 m 500[97] No 2 1957 1957
Sputnik 8A91   Soviet Union RSC Energia 31.1 m 1,327 No 2 1958 1958
SS-520   Japan IHI Aerospace 9.5 m 4[98] No 2[99] 2017[100][l] 2018
Start-1   Russia MITT 22.7 m 532 250 to SSO No 5[101] 1993 2006
Start-1.2   Russia MITT 22.7 m 250-300 to SSO No 1 1997 1997
Start   Russia MITT 28.9 m 300 to SSO No 1 1995 1995
Strela   Russia Khrunichev 24-

27.4 m

1,400[102] No 3[103] 2003 2014
Taurus-1110   United States Orbital

Sciences, Orbital ATK

28.2 m 1180 370 750 to SSO No 3 1994 2000
Taurus-2110   United States Orbital

Sciences, Orbital ATK

29.1 m 1250 375 900 to SSO No 2 1999 2001
Taurus-2210   United States Orbital

Sciences, Orbital ATK

30.9 m 1050 700 to SSO No 1 1998 1998
Taurus-3110   United States Orbital

Sciences, Orbital ATK

30.1 m 1450 445 1,050 to SSO No 2 2009 2011
Taurus-3210[104]   United States Northrop Grumman 27.9 m 1,458[105] N/A 1,054 to SSO[m] No 1 2004 2004
Terran 1   United States Relativity Space 35.2 m 1,250[106] 900 to SSO No 1 2023 2023
Titan II GLV   United States Martin Marietta 33 m 3,600[107] No 11 (+1) 1964 1966
Titan II(23)G   United States Martin Marietta 31.4 m 3,600[108] No 13 1988 2003
Titan IIIA   United States Martin Marietta 38.5 m 3,500 No 4 1964 1965
Titan IIIB   United States Martin Marietta 42 m 3,300 No 22 1966 1969
Titan III(23)B   United States Martin Marietta 42 m 3,350 No 9 1969 1971
Titan III(33)B   United States Martin Marietta 42 m N/A 4,500 No 3 1971 1973
Titan III(24)B   United States Martin Marietta 44 m 4,500 No 23 1971 1984
Titan III(34)B   United States Martin Marietta 45.3 m N/A No 11 1975 1987
Titan IIIC   United States Martin Marietta 41 m 11,500 3,000 No 14 1965 1970
Titan III(23)C   United States Martin Marietta 42.5 m 13,100[109] 3,000 No 22 1970 1982
Titan IIID   United States Martin Marietta 36 m 12,300[110] No 22 1971 1982
Titan IIIE   United States Martin Marietta 48.8 m 15,400[111] No 7 1974 1977
Titan 34D   United States Martin Marietta 44.5 m 14,350 3,600 No 15 1982 1989
Titan IVA   United States Martin Marietta 51.36 m(standard) 17,110[112] 4,944 with IUS 14,090 to SSO[112]

4,536 to GSO with Centaur

3,550 to escape with IUS

No 22[113] 1989 1998
Titan IVB   United States Lockheed Martin 51.36 m(standard) 21,682[114] 5,761[114]

(9,000 with upper stage)

No 17[113] 1997 2005
Tysklon-2

(R-36-O)

  Soviet Union Yuzhmash 32 m 3,350 No 18 1965 1971
Tsyklon-2A   Soviet Union Yuzhmash 39.7 m 3,350[115] No 8[116] 1967 1969
Tsyklon-2M   Soviet Union

  Ukraine

Yuzhmash 39.7 m 2,820[117] No 106[118] 1969 2006[118]
Tsyklon-3   Soviet Union

  Ukraine

Yuzhmash 39.3 m 1,920[119] No 122[120] 1977 2009[120]
Unha-2   North Korea KCST 29.5 m 80 No 1 2009 2009
Unha-3   North Korea KCST 30 m 110 No 4[121] 2009[n] 2016
Vanguard   United States Martin 22.1 m 9[122] No 10 (+1) 1957 1959
Vanguard SLV-7   United States Martin 21.6 m 20 No 1 1959 1959
VLS-1   Brazil AEB, IAE 19.5 m 380[123] No 2[o] 1997 2003
Volna-O   Russia Makeyev 14.2 m 100[124] No 1 (+5)[78] 1995[p] 2005[78]
Voskhod   Soviet Union RSC Energia 44.1 m 5,680 No 299 1963 1976
Vostok-L (Luna)   Soviet Union RSC Energia 30.8 m 4,000 400 to TLI No 9 1958 1960
Vostok (Korabl)   Soviet Union RSC Energia 38.4 m 4,550 390 to TLI[125] No 4 1960 1960
Vostok-K   Soviet Union RSC Energia 30.8 m 2,460[126] No 16 1960 1964
Vostok-2   Soviet Union RSC Energia 30.8 m 4,730[126] No 45 1962 1967
Vostok-2M   Soviet Union RSC Energia 38.8 m 1,300[127] No 93 1964 1991
Soyuz/Vostok   Soviet Union RSC Energia 31 m 6,000[128] No 2 1965 1966
Zenit-2   Soviet Union

  Ukraine

Yuzhnoye 57 m 13,740[129] No 36[130] 1985 2004[131]
Zenit-2FG   Ukraine Yuzhnoye 57 m No 1 2011 2011
Zenit-2M   Ukraine Yuzhnoye 57 m 13,920[129] No 1 2007 2007
Zenit-3F   Ukraine Yuzhnoye 59.6 m 1,740 to GEO[132] No 4[133] 2011 2017
Zenit-3SL   Ukraine Yuzhmash

RSC Energia

59.6 m 7,000[133] 6,160 No 36[133] 1999 2014
Zenit-3SLB   Ukraine Yuzhmash

RSC Energia

59.5 m 3,750[133] No 6[133] 2008 2013
Zhuque-1   China LandSpace 19 m 300[134] 200 to SSO No 1[135] 2018[135] 2018

Retired Atlas rockets edit

Vehicle Origin Manufacturer Height Mass to ... (kg) Reuse Launches

(+ suborbital)

Launch Site (s) Date of flight
LEO GTO Other First Last
Atlas-Able   United States General Dynamics 28 m ~175 to TLI No 3 1959 1960
Atlas-Agena   United States Convair/General Dynamics 36 m 1,000 390 to TLI No 109 1960 1978
Atlas-Centaur   United States Lockheed 36.2-38.8 m 1,134[136] 2,222[137] No 148 1962 1983
Atlas B   United States Lockheed Martin 24.9 m ~4,000 No 10 1958 1959
Atlas-D OV1   United States Convair/General Dynamics 25.9 m 1,400 No 7 1965 1967
Atlas E/F-Agena   United States Convair/General Dynamics/Lockheed 34 m 1,000 390 to TLI No 1 1978 1978
Atlas E/F-Altair-3A   United States Convair/General Dynamics 27.3 m 210 No 1 1990 1990
Atlas E/F-Burner-2   United States Convair/General Dynamics 28.9 m 950 No 1 1972 1972
Atlas E/F-MSD   United States Convair/General Dynamics 27.3 m 800 No 4 1976 1980
Atlas E/F-OIS   United States Convair/General Dynamics 28.7 m 870 No 2 1979 1985
Atlas E/F-OV1   United States Convair/General Dynamics 26.5 m 363 No 4 1968 1971
Atlas E/F-PTS   United States Convair/General Dynamics 26.5 m 295 No 1 1974 1974
Atlas E/F-SGS-1   United States Convair/General Dynamics 29 m 450 No 8 1977 1981
Atlas E/F-SGS-2   United States Convair/General Dynamics 29 m 770 No 4 1983 1985
Atlas E/F-Star-17A   United States Convair/General Dynamics 27.4 m N/A 800 to MPEO No 1 1975 1975
Atlas E/F-Star-37S   United States Convair/General Dynamics 29 m N/A 1,100 to SSO No 19 1978 1995
Atlas-F Agena-D   United States Convair/General Dynamics 34 m N/A 2,300 to Polar No 1 1978 1978
Atlas G   United States Lockheed 43.9 m 5,900[138] 2,222 1,179 to HCO[138] No 7[138] 1984 1989
Atlas H MSD   United States Lockheed 27 m 3,630[139] No 5 1983 1987
Atlas LV-3B   United States Convair 28.7 m 1,360 No 9 1960 1963
Atlas SLV-3   United States Convair 33.3 m No 63 1966 1983
Atlas SLV-3 Burner-2   United States Convair 30.3 m ~1,000 No 1 1968 1968
Atlas I   United States Lockheed Martin 43.9 m 5,900[138] 2,340[138] No 11[138] 1990 1997
Atlas II   United States Lockheed Martin 47.5 m 6,780[138] 2,810 2,000 to HCO[138] No 10[138] 1991 1998
Atlas IIA   United States Lockheed Martin 47.5 m 7,316[138] 3,180 2,160 to HCO[138] No 23[138] 1992 2002
Atlas IIAS   United States Lockheed Martin 49 m 8,618[138] 3,833 2,680 to HCO[138] No 30[138] 1993 2004
Atlas IIIA   United States Lockheed Martin 52.5 m 8,686[138] 4,060 2,970 to HCO[138] No 2[138] 2000 2004
Atlas IIIB/DEC   United States Lockheed Martin 53.7 m 10,759[138] 4,609[138] No 1[138] 2002 2002
Atlas IIIB/SEC   United States Lockheed Martin 54.7 m 10,218[140] 4,193[138] No 3[138] 2003 2005
Atlas V 401   United States ULA 57.3 m 9,050[141] 4,950 6,670 to SSO No 41[141] 2002 2022
Atlas V 411   United States ULA 58.2 m 9,050[141] 6,075 8,495 to SSO No 6[141] 2006 2020
Atlas V 421   United States ULA 59.1 m 9,050[141] 7,000 9,050 to SSO No 9[141] 2007 2022
Atlas V 431   United States ULA 59.1 m 9,050[141] 7,800 9,050 to SSO No 3[141] 2005 2016
Atlas V 501   United States ULA 62.5 m 8,250[141] 3,970 5,945 to SSO
1,500 to GEO 		No 8[141] 2010 2023
Atlas V 511   United States ULA 62.5 m 11,000[141] 5,250 7,820 to SSO

1,750 to GEO

No 1[142] 2022 2022
Atlas V 521   United States ULA 59.7 m 13,300[141] 6,485 9,585 to SSO

2,760 to GEO

No 2[141] 2003 2004
Atlas V 531   United States ULA 59.7 m 15,300[141] 7,425 11,160 to SSO

3,250 to GEO

No 5[141] 2010 2022
Atlas V 541   United States ULA 59.7 m 17,100[141] 8,240 12,435 to SSO

3,730 to GEO

No 9[141] 2011 2022

Retired Delta rockets edit

Vehicle Origin Manufacturer Height Mass to ... (kg) Reuse Launches

(+ suborbital)

Launch Site (s) Date of flight
LEO GTO Other First Last
Delta 0300   United States McDonnell Douglas 34 m 340[143] 747 to SSO[144] No 3[145] 1972 1973[146]
Delta 0900   United States McDonnell Douglas 34 m 1,300[147] 818 to SSO[145] No 2[145] 1972 1972
Delta 1410   United States McDonnell Douglas 35.2 m 340[148] No 1[145] 1975 1975
Delta 1604   United States McDonnell Douglas 35.2 m 390[149] No 2[145] 1972 1973
Delta 1900   United States McDonnell Douglas 35.2 m 1,800[145] No 1[145] 1973 1973
Delta 1910   United States McDonnell Douglas 35.2 m 1,066[150] No 1[145] 1975 1975
Delta 1913   United States McDonnell Douglas 35.2 m 328[151] No 1[145] 1973 1973
Delta 1914   United States McDonnell Douglas 35.2 m 680[152] No 2[145] 1972 1973
Delta 2310   United States McDonnell Douglas 35.2 m 336[153] No 3[145] 1974 1981
Delta 2313   United States McDonnell Douglas 35.2 m 243 to GEO[154] No 3[145] 1974 1977
Delta 2910   United States McDonnell Douglas 35.2 m 1,887[145] No 6[145] 1975 1978
Delta 2913   United States McDonnell Douglas 35.2 m 2,000[155] 700[155] No 6[145] 1975 1976
Delta 2914   United States McDonnell Douglas 35.2 m 724[145] No 30[145] 1974 1979
Delta 3910   United States McDonnell Douglas 35.2 m 2,494[145] 1,154 with PAM-D No 10[145] 1980 1988
Delta 3913   United States McDonnell Douglas 35.2 m 816[156] No 1[145] 1981 1981
Delta 3914   United States McDonnell Douglas 35.2 m 954[145] No 13[145] 1975 1987
Delta 3920   United States McDonnell Douglas 35.2 m 3,452[145] 1,284 with PAM-D No 10[145] 1982 1989
Delta 3924   United States McDonnell Douglas 35.2 m 1,104[145] No 4[145] 1982 1984
Delta 4925   United States McDonnell Douglas 35.2 m 3,400[157] 1,312[145] No 2[145] 1989 1990
Delta 5920   United States McDonnell Douglas 35.2 m 3,848[158] No 1[145] 1989 1989
Delta II 6920   United States McDonnell Douglas 38.8 m 3,983[145] No 3[145] 1990 1992
Delta II 6925   United States McDonnell Douglas 39.4 m 1,447 1,447[145] No 14[145] 1989 1992
Delta II 7320   United States Boeing IDS / ULA 38.9 m 2,865[145] 1,651 to SSO No 12[145] 1999 2015
Delta II 7326   United States Boeing IDS 38.4 m 934[145] 636 to TLI

629 to HCO

No 3[145] 1998 2001
Delta II 7420   United States ULA 39 m 3,185[145] 1,966 to SSO No 14[145] 1998 2018
Delta II 7425   United States Boeing IDS 39 m 1,100[145] 804 to HCO No 4[145] 1998 2002
Delta II 7426   United States Boeing IDS 39 m 1,058[145] 734 to TLI

711 to HCO

No 1[145] 1999 1999
Delta II 7920   United States Boeing IDS / ULA 39.4 m 5,030[145] 3,123 to SSO No 29[145] 1998 2017
Delta II 7925   United States Boeing IDS / ULA 39.4 m 1,819[145] 1,177 to TLI

1,265 to HCO

No 69[145] 1990 2009
Delta II-H 7920H   United States Boeing IDS / ULA 39 m 6,097[145] No 3[145] 2003 2011
Delta II-H 7925H   United States Boeing IDS / ULA 39.8 m 2,171 1,508 to HCO[145] No 3[145] 2003 2007
Delta III 8930   United States Boeing IDS 39 m 8,292[145] 3,810 No 3[145] 1998 2000
Delta IV Heavy   United States ULA 72 m 28,370[159] 14,210[159] 23,560 to polar [159]

11,290 to TLI 8,000 to TMI

No 16[160] 2004 2024
Delta IV M   United States Boeing IDS 61.3 m 9,440[159] 4,440 7,690 to polar No 3[160] 2003 2006
Delta IV M+(4,2)   United States ULA 61.3 m 13,140[159] 6,390 10,250 to polar No 14[160] 2002 2019
Delta IV M+(5,2)   United States ULA 65.5 m 11,470[159] 5,490 9,600 to polar No 3[160] 2012 2018
Delta IV M+(5,4)   United States ULA 65.5 m 14,140[159] 7,300 11,600 to polar No 8[160] 2009 2019

Retired Thor rockets edit

Vehicle Origin Manufacturer Height Mass to ... (kg) Reuse Launches

(+ suborbital)

Launch Site (s) Date of flight
LEO GTO Other First Last
Thor-Able I   United States Douglas/Aerojet 26.9 m 250 No 3 1958 1958
Thor-Able II   United States Douglas/Aerojet 27.3 m 270 No 4 1959 1960
Thor-Able III   United States Douglas/Aerojet 27.4 m ~64 to HEO No 1 1959 1959
Thor-Able IV   United States Douglas/Aerojet 27.2 m ~43 to Heliocentric No 1 1960 1960
Thor Agena-A   United States Douglas/Lockheed 22.7 m 860 No 16 1959 1960
Thor Agena-B   United States Douglas/Lockheed 26.3 m 1,200 No 21 1962 1965
Thor Agena-D   United States Douglas/Lockheed 29.3 m 1,150 No 22 1962 1967
Thorad SLV-2G Agena D   United States Douglas/Lockheed 32.9 m 2,000 No 30 1966 1971
Thorad SLV-2H Agena D   United States Douglas/Lockheed 34 m 2,000 No 13 1969 1972
Thor-Burner-1 MG-18   United States Douglas 23 m 770 150-300 to MEO No 2 1965 1965
Thor-Burner-1 Altair-3   United States Douglas ~24 m >73 No 4 1965 1966
Thor-Burner-2   United States Douglas 22.4 m 250 to MEO No 12 1966 1971
Thor-Burner-2A   United States Douglas 23.5 m 300 to MEO No 8 1971 1976
Thor-Delta   United States Douglas 31 m 226 45 No 12 1960 1962
Thor-Delta A   United States Douglas 31 m 250 68 No 2 1962 1962
Thor-Delta B   United States Douglas 31 m 370 68 No 9 1962 1964
Thor-Delta C   United States Douglas 27.5 m 81 No 11 1963 1967
Thor-Delta C1   United States Douglas 27.5 m 81 No 2 1966 1969
Thor-Delta D   United States Douglas 32 m 450 104 No 2 1964 1965
Thor-Delta E   United States Douglas 31 m 540 150 No 6 1965 1967
Thor-Delta E1   United States Douglas 28 m 540 205 No 17 1966 1971
Thor-Delta G   United States Douglas 30 m 650 No 2 1966 1967
Thor-Delta J   United States Douglas 31 m 260 263 No 1 1968 1968
Thor-Delta L   United States Douglas 35 m 356 300 No 2 1969 1972
Thor-Delta M   United States Douglas 34 m 356 355 No 12 1968 1971
Thor-Delta M6   United States Douglas 32.4 m 454 450 No 1 1971 1971
Thor-Delta N   United States Douglas 33 m 900 No 6 1968 1972
Thor-Delta N6   United States Douglas 33 m 1,600 No 3 1970 1971
Thor-DM21 Able-Star   United States Douglas/Aerojet 29 m 150 No 11 1960 1962
Thor-DSV2A Able-Star   United States Douglas/Aerojet 29 m 150 No 8 1963 1965
Thor-ISS   United States Douglas/Thiokol 23 m 500 to MEO No 5 1976 1980
Thor-SLV2A Agena-B   United States Douglas/Lockheed 31 m 400 No 2 1963 1966
Thor-SLV2A Agena-D   United States Douglas/Lockheed 29.3 m 1,500 No 60 1963 1968

Notes edit

  1. ^ Reference altitude 500 km
  2. ^ First suborbital test in 1969, first orbital launch attempt in 1970
  3. ^ a b Despite not being officially acknowledged by the manufacturer, significant changes between different iterations of the rocket lead to the identification of different variants.[15]
  4. ^ Without Buran, and assuming payload providing orbital insertion
  5. ^ 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.
  6. ^ 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.
  7. ^ Despite not being officially acknowledged by the manufacturer, significant changes between different iterations of the rocket lead to the identification of different variants.[39]
  8. ^ Suborbital test flights in 1995, 1997 and 2002, no orbital launches attempted
  9. ^ 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.
  10. ^ A suborbital test flight was conducted in May 2018.[61]
  11. ^ 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.
  12. ^ 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.[98]
  13. ^ Reference altitude 400 km
  14. ^ 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.[121]
  15. ^ A third rocket exploded before launch.
  16. ^ First orbital launch attempt in 2005

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