- Comparison of orbital launch systems
-
This page exposes the full list of orbital launch systems.
For the short simple list of launchers families, see Comparison of orbital launchers families.
Orbital launch systems are rockets and other systems capable of placing payloads into or beyond Earth orbit.
Legend for below table: [under development] — [retired] — [operational]Vehicle Origin Manufacturer Mass to
LEO
(kg)Mass to
other orbits
(kg)Cost
(Mil US$)Cost/kg
(LEO) (US$)Launches Status First flight Last flight Vehicle Angara 1.1 Russia Khrunichev 0 Development Angara 1.1 Angara 1.2 Russia Khrunichev [1] 3,8000 Development Angara 1.2 Angara A3 Russia Khrunichev [1] 14,600[1] 2,400–3,600 to GTO[2] €50 (US$70)0 Development Angara A3 Angara A5 Russia Khrunichev [3][4] 24,500 (63°)0 Development Angara A5 Angara A7 Russia Khrunichev [3][4] 41,0000 Development Angara A7 Ariane 1 Europe Aérospatiale 1,400 [5] 1,830 to GTO[5] 11Retired 1979 1986 Ariane 1 Ariane 2 Europe Aérospatiale [5] 2,270 to GTO[5] 6Retired 1986 1989 Ariane 2 Ariane 3 Europe Aérospatiale [5] 2,650 to GTO[5] 11Retired 1984 1989 Ariane 3 Ariane 4 40 Europe Aérospatiale [5] 4,600 2,740 to SSO
1,900 to GTO[5][5] 3Retired 1990 1993 Ariane 4 40 Ariane 4 40 H10+ Europe Aérospatiale [5] 2,020 to GTO[5] 1Retired 1995 1995 Ariane 4 40 H10+ Ariane 4 40 H10-3 Europe Aérospatiale [5] 2,105 to GTO[5] 3Retired 1995 1999 Ariane 4 40 H10-3 Ariane 4 42L Europe Aérospatiale [5] 7,000 4,500 to SSO
3,200 to GTO[5][5] 1Retired 1993 1993 Ariane 4 42L Ariane 4 42L H10+ Europe Aérospatiale [5] 7,000[5] 3,350 to GTO[5] 1Retired 1994 1994 Ariane 4 42L H10+ Ariane 4 42L H10-3 Europe Aérospatiale [5] 7,000[5] 3,480 to GTO[5] 11Retired 1995 2002 Ariane 4 42L H10-3 Ariane 4 42P Europe Aérospatiale [5] 6,000 3,400 to SSO
2,600 to GTO[5][5] 2Retired 1990 1992 Ariane 4 42P Ariane 4 42P H10+ Europe Aérospatiale [5] 2,740 to GTO[5] 4Retired 1992 1994 Ariane 4 42P H10+ Ariane 4 42P H10-3 Europe Aérospatiale [5] 2,930 to GTO[5] 9Retired 1994 2002 Ariane 4 42P H10-3 Ariane 4 44L Europe Aérospatiale [5] 7,000 6,000 to SSO
4,200 to GTO[5][5] 11Retired 1989 1992 Ariane 4 44L Ariane 4 44L H10+ Europe Aérospatiale [5] 7,000[5] 4,460 to GTO[5] 5Retired 1992 1994 Ariane 4 44L H10+ Ariane 4 44L H10-3 Europe Aérospatiale [5] 7,000[5] 4,720 to GTO[5] 24Retired 1995 2003 Ariane 4 44L H10-3 Ariane 4 44LP Europe Aérospatiale [5] 7,000 5,000 to SSO
3,700 to GTO[5][5] 7Retired 1988 1993 Ariane 4 44LP Ariane 4 44LP H10+ Europe Aérospatiale [5] 7,000[5] 4,030 to GTO[5] 6Retired 1992 1995 Ariane 4 44LP H10+ Ariane 4 44LP H10-3 Europe Aérospatiale [5] 7,000[5] 4,220 to GTO[5] 13Retired 1995 2001 Ariane 4 44LP H10-3 Ariane 4 44P Europe Aérospatiale [5] 6,500 4,100 to SSO
3,000 to GTO[5][5] 2Retired 1991 1991 Ariane 4 44P Ariane 4 44P H10-3 Europe Aérospatiale [5] 3,465 to GTO[5] 9Retired 1995 2001 Ariane 4 44P H10-3 Ariane 5ECA Europe EADS Astrium [6] 21,000[7] [8] 220[8] 10,476 31
[note 1]Operational 2002 Ariane 5ECB Europe EADS Astrium 21,000 to GTO 0 Development Ariane 5ECB Ariane 5ES Europe EADS Astrium [6] 21,0008,000 to GTO[9] [8] 220[8] 10,4762 Operational 2008 Ariane 5ES Ariane 5G Europe EADS Astrium [9] 18,000[9] 6,900[9] 16Retired[10] 1996 2003 Ariane 5G Ariane 5G+ Europe EADS Astrium citation needed] 18,000[[9] 7,100 to GTO[9] 3Retired[10] 2004 2004 Ariane 5G+ Ariane 5GS Europe EADS Astrium citation needed] 18,000[[9] 6,600 to GTO[9] 6Retired[10] 2005 2009 Ariane 5GS ASLV India ISRO citation needed] 4[Retired[citation needed] 1987 1994 ASLV Athena I United States Lockheed Martin [11] 4Retired 1995 2001 Athena I Athena Ic [12] United States ATK
Lockheed Martin0 Development Athena Ic Athena II United States Lockheed Martin citation needed] 2,065[[13] 3Retired[citation needed] 1998 1999 Athena II Athena IIc [12] United States ATK
Lockheed Martin0 Development Athena IIc Atlas-Centaur United States Lockheed Retired[citation needed] 1962 1983 Atlas-Centaur Atlas G United States Lockheed [14] 5,900 2,222 to GTO
1,179 to HCO[14][14] 7Retired 1984 1989 Atlas G Atlas H/MSD United States Lockheed 5 Retired 1983 1987 Atlas H/MSD Atlas I United States Lockheed Martin [14] 5,900[14] 2,340[14] 11Retired 1990 1997 Atlas I Atlas II United States Lockheed Martin [14] 6,780 2,810 to GTO
2,000 to HCO[14][14] 10Retired 1991 1998 Atlas II Atlas IIA United States Lockheed Martin [14] 7,316 3,180 to GTO
2,160 to HCO[14][14] 23Retired 1992 2002 Atlas IIA Atlas IIAS United States Lockheed Martin [14] 8,618 3,833 to GTO
2,680 to HCO[14][14] 30Retired 1993 2004 Atlas IIAS Atlas IIIA United States Lockheed Martin [14] 8,686 4,060 to GTO
2,970 to HCO[14][14] 2Retired 2000 2004 Atlas IIIA Atlas IIIB/DEC United States Lockheed Martin [14] 10,759[14] 4,609 to GTO[14] 1Retired 2002 2002 Atlas IIIB/DEC Atlas IIIB/SEC United States Lockheed Martin [14] 4,193 to GTO[14] 3Retired 2003 2005 Atlas IIIB/SEC Atlas V 401 United States United Launch Alliance [15] 9,050 6,670 to SSO
4,950 to GTO[15][8] 125[8] 13,812[15] 11Operational 2002 Atlas V 401 Atlas V 411 United States United Launch Alliance [15] 9,050 8,495 to SSO
6,075 to GTO[15][15] 3Operational 2006 Atlas V 411 Atlas V 421 United States United Launch Alliance [15] 9,050 9,050 to SSO
7,000 to GTO[15][15] 3Operational 2007 Atlas V 421 Atlas V 431 United States United Launch Alliance [15] 9,050 9,050 to SSO
7,800 to GTO[15][15] 2Operational 2005 Atlas V 431 Atlas V 501 United States United Launch Alliance [15] 8,250 5,945 to SSO
3,970 to GTO
1,500 to GEO[15][15] 3Operational 2010 Atlas V 501 Atlas V 511 United States United Launch Alliance [15] 10,950 7,820 to SSO
5,370 to GTO
1,750 to GEO[15][15] 0Operational Atlas V 511 Atlas V 521 United States United Launch Alliance [15] 13,300 9,585 to SSO
6,485 to GTO
2,760 to GEO[15][15] 2Operational 2003 Atlas V 521 Atlas V 531 United States United Launch Alliance [15] 15,300 11,160 to SSO
7,425 to GTO
3,250 to GEO[15][15] 1Operational 2010 Atlas V 531 Atlas V 541 United States United Launch Alliance [15] 17,100 12,435 to SSO
8,240 to GTO
3,730 to GEO[15][15] 0Operational Atlas V 541 Atlas V 551 United States United Launch Alliance [15] 18,500 12,435 to SSO
8,700 to GTO
3,960 to GEO[15][15] 1Operational 2006 Atlas V 551 Black Arrow United Kingdom RAE 73 2(+2) Retired[citation needed] 1969[note 2] 1971 Black Arrow Commercial Titan III United States Martin Marietta 4 Retired 1990 1992 Commercial Titan III Delta 0300 United States McDonnell Douglas 700 370 to SSO [16] 3Retired[17] 1972 1973 Delta 0300 Delta 0900 United States McDonnell Douglas [18] 1,300[16] 818 to SSO[16] 2Retired 1972 1972 Delta 0900 Delta 1410 United States McDonnell Douglas [16] 1Retired 1975 1975 Delta 1410 Delta 1604 United States McDonnell Douglas [16] 2Retired 1972 1973 Delta 1604 Delta 1900 United States McDonnell Douglas [16] 1,800[16] 1Retired 1973 1973 Delta 1900 Delta 1910 United States McDonnell Douglas [16] 1Retired 1975 1975 Delta 1910 Delta 1913 United States McDonnell Douglas [16] 1Retired 1973 1973 Delta 1913 Delta 1914 United States McDonnell Douglas [16] 2Retired 1972 1973 Delta 1914 Delta 2310 United States McDonnell Douglas [16] 3Retired 1974 1981 Delta 2310 Delta 2313 United States McDonnell Douglas [16] 3Retired 1974 1977 Delta 2313 Delta 2910 United States McDonnell Douglas [16] 1,887[16] 6Retired 1975 1978 Delta 2910 Delta 2913 United States McDonnell Douglas [19] 2,000[19] 700 to GTO[16] 6Retired 1975 1976 Delta 2913 Delta 2914 United States McDonnell Douglas [16] 724 to GTO[16] 30Retired 1974 1979 Delta 2914 Delta 3910 United States McDonnell Douglas [16] 2,494[16] 1,154 to GTO with PAM-D[16] 10Retired 1980 1988 Delta 3910 Delta 3913 United States McDonnell Douglas [16] 1Retired 1981 1981 Delta 3913 Delta 3914 United States McDonnell Douglas [16] 954 to GTO[16] 13Retired 1975 1987 Delta 3914 Delta 3920 United States McDonnell Douglas [16] 3,452[16] 1,284 to GTO with PAM-D[16] 10Retired 1982 1989 Delta 3920 Delta 3924 United States McDonnell Douglas [16] 1,104 to GTO[16] 4Retired 1982 1984 Delta 3924 Delta 4925 United States McDonnell Douglas [20] 3,400[16] 1,312 to GTO[16] 2Retired 1989 1990 Delta 4925 Delta 5920 United States McDonnell Douglas [21] 3,848[16] 1Retired 1989 1989 Delta 5920 Delta II 6920 United States McDonnell Douglas [16] 3,983[16] 3Retired 1990 1992 Delta II 6920 Delta II 6925 United States McDonnell Douglas [16] 1,447 to GTO[16] 14Retired 1989 1992 Delta II 6925 Delta II 7320 United States United Launch Alliance [note 3][16] 2,865[note 3][16] 1,651 to SSO[16] 10Retired 1999 2011 Delta II 7320 Delta II 7326 United States Boeing IDS 934 to GTO
636 to TLI
629 to HCO[note 3][16][16] 3Retired 1998 2011[citation needed] Delta II 7326 Delta II 7420 United States United Launch Alliance [note 3][16] 3,185[note 3][16] 1,966 to SSO[16] 13Retired 1998 2010 Delta II 7420 Delta II 7425 United States Boeing IDS 1,100 to GTO
804 to HCO[note 3][16][16] 4Retired 1998 2002 Delta II 7425 Delta II 7426 United States Boeing IDS 1,058 to GTO
734 to TLI
711 to HCO[note 3][16][16] 1Retired 1999 1999 Delta II 7426 Delta II 7920 United States United Launch Alliance [note 3][16] 5,030[note 3][16] 3,123 to SSO[16] 27Operational 1998 Delta II 7920 Delta II 7925 United States Boeing IDS 1,819 to GTO
1,177 to TLI
1,265 to HCO[note 3][16][16] 69Retired 1990 2009 Delta II 7925 Delta II-H 7920H United States United Launch Alliance [note 3][16] 6,097[16] 3Retired 2003 2011 Delta II-H 7920H Delta II-H 7925H United States United Launch Alliance 2,171 to GTO
1,508 to HCO[note 3][16][16] 3Operational
[citation needed][note 4]2003 Delta II-H 7925H Delta III 8930 United States Boeing IDS [16] 8,292[16] 3,810 to GTO[16] 3Retired 1998 2000 Delta III 8930 Delta IV-H United States United Launch Alliance [22] 22,950[22] 12,980 to GTO[23] US$300 (€220)5 Operational 2004 Delta IV-H Delta IV-M United States Boeing IDS [24] 8,120 4,210 to GTO
2,722 to escape[24][24] 3Retired 2003 2006 Delta IV-M Delta IV-M+(4,2) United States United Launch Alliance [25] 11,750[25] 5,740 to GTO[24] 8Operational 2002 Delta IV-M+(4,2) Delta IV-M+(5,2) United States United Launch Alliance [25] 10,250[25] 4,590 to GTO[24] 0Operational Delta IV-M+(5,2) Delta IV-M+(5,4) United States United Launch Alliance [25] 13,500[25] 16,470 to GTO[24] 1Operational 2009[26] Delta IV-M+(5,4) Diamant France SEREB Retired 1965 1975 Diamant Dnepr-1 Ukraine Yuzhmash [27] 3,700[2] €10 (US$14)16 Operational 1999 Dnepr-1 Energia[note 5] Soviet Union NPO Energia [28] 100,000GTO[28] 20,000 to
32,000 to TLI[28][note 6] 240[29] 1Retired 1987 1987 Energia Energia-Buran Soviet Union NPO Energia (Launcher)
NPO Molniya (Orbiter)[28] 30,000
[note 7]1 Retired 1988 1988 Energia-Buran Epsilon Japan IHI Aerospace[30] [31] 1,2000 Development[31] Epsilon Falcon 1 United States SpaceX 670 7 5 Retired[32] 2006 2009 Falcon 1 Falcon 1e United States SpaceX 1,010 10.9 10,792 0 Development[32] Falcon 1e Falcon 9 United States SpaceX [33][34] 10,450[33] 4,680 to GTO[33] 565,359 2 Operational 2010 Falcon 9 Falcon Heavy United States SpaceX [35] 53,000[35] 19,000 to GTO
16,000 to TLI[35]80–125 2,204 0 Development Falcon Heavy GSLV Mk.I(a) India ISRO 5,100 1,500 to GTO 1 Retired
[citation needed]2001 2001 GSLV Mk.I(a) GSLV Mk.I(b) India ISRO 1,900 4 Retired
[citation needed]2004 2007 GSLV Mk.I(b) GSLV Mk.I(c) India ISRO 1 Operational 2010 GSLV Mk.I(c) GSLV Mk.II India ISRO [36] 2,5001 Operational 2010 GSLV Mk.II GSLV Mk.III India ISRO[37] 10,000 [38] 4,500–5,0000 Development GSLV Mk.III H-I Japan
United StatesMitsubishi Heavy Industries 3,200 1,100 to GTO 9 Retired 1986 1992 H-I H-II Japan Mitsubishi Heavy Industries [39][note 8] 5Retired 1994 1998 H-II H-IIA 202 Japan Mitsubishi Heavy Industries [40] 10,000[40] 3,800 to GTO[40] 7Operational 2001 H-IIA 202 H-IIA 204 Japan Mitsubishi Heavy Industries [40] 5,800 to GTO[40] 1Operational 2006 H-IIA 204 H-IIA 2022 Japan Mitsubishi Heavy Industries [40] 4,200[40] 3Retired 2005 2007 H-IIA 2022 H-IIA 2024 Japan Mitsubishi Heavy Industries [40] [40] 7Retired 2002 2008 H-IIA 2024 H-IIB 304 Japan Mitsubishi Heavy Industries [41] 19,000[42] 8,000[43] 2Operational 2009 H-IIB 304 H-II/SSB Japan Mitsubishi Heavy Industries [39] 1Retired 1995 1995 H-II/SSB H-IIS Japan Mitsubishi Heavy Industries [note 9][39] 1Retired 1999 1999 H-IIS Haas Romania ARCA 0 Development Haas J-I Japan IHI Corporation
Nissan Motors[44]0(+1) Retired 1996 1996 J-I Kaituozhe-1 China CALT citation needed] 50[2 Operational[citation needed] 2002 Kaituozhe-1 Kosmos-3M Russia NPO Polyot 1,500 €12 million[2] 442 Operational 1967 Kosmos-3M Lambda 4S Japan Nissan Motors[44] [31] 265 Retired 1966 1970 Lambda 4S Long March 1 China CALT 300 3 Retired[45] 1969 1971 Long March 1 Long March 1D China CALT 0(+3) Operational[citation needed] 1995[note 10] Long March 1D Long March 2A China CALT 1,800 1 Retired 1974 1974 Long March 2A Long March 2C China CALT 2,400 32 Operational 1975 Long March 2C Long March 2D China CALT 3,500 14 Operational 1992 Long March 2D Long March 2E China CALT 7 Retired 1990 1995 Long March 2E Long March 2F China CALT 8,400 3,370 7 Operational 1999 Long March 2F Long March 2F/G China CALT 1 Operational 2011 Long March 2F/G Long March 3 China CALT 5,000 1,340 14 Retired 1984 2000 Long March 3 Long March 3A China CALT citation needed] 8,500[[46] 2,650 to GTOOperational 1994 Long March 3A Long March 3B China CALT [47] 12,00010 Operational 1996 Long March 3B Long March 3B/E China CALT 4 Operational 2007 Long March 3B/E Long March 3B(A) China CALT 0 Development Long March 3B(A) Long March 3C China CALT [48] 3,700 4
[citation needed]Operational 2008 Long March 3C Long March 4A China CALT 2
[citation needed]Retired 1988 1990 Long March 4A Long March 4B China CALT 4,200 citation needed] 1,500 to GTO[ 11
[citation needed]Operational 1999 Long March 4B Long March 4C China CALT citation needed] 4,200[citation needed] 1,500 to GTO[Operational 2007 Long March 4C Long March 5 China CALT [49] 25,000[49] 14,000 to GTO0 Development Long March 5 Long March 6 China CALT 0 Development
since 2009Long March 6 Long March 7 China CALT SSO[citation needed] 500 to0 Development
since 2009Long March 7 M-V Japan Nissan Motors[44] (-2000)
IHI AEROSPACE[30] (-2006)[31] 1,800 - 1,8507 Retired 1997 2006 M-V Minotaur I United States Orbital [50] 10Operational 2000 2011 Minotaur I Minotaur IV United States Orbital citation needed] 1,735[2(+2) Operational 2010 Minotaur IV Minotaur V United States Orbital 640 to GTO
447 to TLI0 Development Minotaur V Molniya Soviet Union RSC Energia Retired 1960 1964 Molniya Molniya-M Soviet Union
RussiaRSC Energia 275 Retired 1964 2010 Molniya-M Mu-3C Japan Nissan Motors[44] [31] 1954 Retired 1974 1979 Mu-3C Mu-3H Japan Nissan Motors[44] [31] 3003 Retired 1977 1978 Mu-3H Mu-3S Japan Nissan Motors[44] [31] 3004 Retired 1980 1984 Mu-3S Mu-3SII Japan Nissan Motors[44] [31] 7708 Retired 1985 1995 Mu-3SII Mu-4S Japan Nissan Motors[44] [31] 1804 Retired 1971 1972 Mu-4S N1 Soviet Union NPO Energia [51][52][53][note 11] 95,000[54] 4Retired 1969 1972 N1 N-I Japan
United StatesMitsubishi Heavy Industries citation needed] 1,200[citation needed] 360 to GTO[Retired[citation needed] 1975 1982 N-I N-II Japan
United StatesMitsubishi Heavy Industries citation needed] 2,000[citation needed] 730[8 Retired 1981 1987 N-II Naro-1 South Korea
RussiaKARI/Khrunichev citation needed] 100[citation needed] 2[Development[citation needed] 2009 2010 Naro-1 Paektusan North Korea KCST citation needed] 1[Retired[citation needed] 1998 1998 Pegasus United States Orbital 443 citation needed] 40[Operational 1990 2008 Pegasus Polyot Soviet Union RSC Energia 1,400 citation needed] 2[Retired[citation needed] 1963 1964 Polyot Proton Soviet Union
RussiaKhrunichev [55] 21,600[55] 6,360 to GTO[56] 85[56] 4,302[57] 335Operational 1965 Proton PSLV India ISRO [58] 3,200 1,600 to SSO
1,050 to GTO[59]17 11 Operational 1993 PSLV PSLV-CA India ISRO [58] 2,800[59] 1,100 to SSO17 6 Operational 2007 PSLV-CA PSLV-XL India ISRO [59] 3,800 1,750 to SSO
1,300 to GTO[59]2 Operational 2008 PSLV-XL PSLV-HP India ISRO [59] 4,000 1,900 to SSO
1,440 to GTO[59]0 Development PSLV-HP Rokot Russia Khrunichev 1,950 [60] 14[61] 14Operational 1990 Safir Iran Iranian Space Agency 3 Operational[citation needed] 2008 Safir Saturn I United States Chrysler (S-I)
Douglas (S-IV) 10
[citation needed]Retired 1961 1965 Saturn I Saturn IB United States Chrysler (S-IB)
Douglas (S-IVB)citation needed] 20,412[[62] 9Retired 1966 1975 Saturn IB Saturn V United States Boeing (S-IC)
North American (S-II)
Douglas (S-IVB)[63] 118,000[63] 47,000 to TLI[64] 185 (1.11 billion in 2011)[65][66][note 12] 13Retired 1967 1973 Saturn V Scout United States US Air Force/NASA 150 Retired[citation needed] 1961 1994 Scout Shavit Israel IAE 160 15 9 Operational 1988 Shavit Shtil' Russia Makeyev 160 - 430 Operational[citation needed] 1998 Shtil' Simorgh Iran Iranian Space Agency [67][68] 60-1000 Development[citation needed] Simorgh SLS United States Alliant Techsystems (SRBs)
130,000[70] 70,000 —0 Development SLS SLV India ISRO 40 4 Retired[citation needed] 1979 1983 SLV Soyuz Soviet Union RSC Energia 6,450 30 Retired 1966 1975 Soyuz Soyuz-L Soviet Union RSC Energia 5,500 3 Retired 1970 1971 Soyuz-L Soyuz-M Soviet Union RSC Energia 6,600 Retired 1971 1976 Soyuz-M Soyuz-U Soviet Union
RussiaTsSKB-Progress Plesetsk) 6,200–6,700 kg from
6590-6950 from Baikonour[71]Operational 1973 Soyuz-U Soyuz-U2 Soviet Union
RussiaTsSKB-Progress Retired 1982 1995 Soyuz-U2 Soyuz-FG Russia TsSKB-Progress [72] 6,790–7130 kgOperational 2001 Soyuz-FG Soyuz-2.1a Russia TsSKB-Progress 7(+1) Operational 2004[note 13] Soyuz-2.1a Soyuz-2.1b Russia TsSKB-Progress 4 Operational 2011 Soyuz-2.1b Soyuz-2.1v Russia TsSKB-Progress 2,850 0 Development Soyuz-2.1v Space Shuttle United States Alliant Techsystems (SRBs)
Martin Marietta (ET)
Rockwell International (Orbiter)[note 7] 24,400[56] 300[56] 10,416[73] 135Retired 1981 2011 Space Shuttle Sputnik 8K71PS Soviet Union RSC Energia 500 2 Retired[citation needed] 1957 1957 Sputnik 8K71PS Sputnik 8A91 Soviet Union RSC Energia 1,327 Retired[citation needed] 1958 1958 Sputnik 8A91 Start-1 Russia MITT 532 167 to SSO Operational[citation needed] 1993 Start-1 Strela Russia Khrunichev 1,700 €5 million.[2] Operational[citation needed] 2003 Strela Taurus United States Orbital 1,320 Operational[citation needed] 1994 2011 Taurus Taurus II United States Orbital Sciences Corporation [74] 6,000[74] 1,900 to GTO0 Development Taurus II Titan II GLV United States Martin Marietta 11(+1) Retired 1964 1966 Titan II GLV Titan II(23)G United States Martin Marietta Retired 1988 2003 Titan II(23)G Titan IIIA United States Martin Marietta Retired 1964 1965 Titan IIIA Titan IIIB United States Martin Marietta 70 Retired 1966 1987 Titan IIIB Titan IIIC United States Martin Marietta 36 Retired 1965 1982 Titan IIIC Titan IIID United States Martin Marietta 22 Retired 1971 1982 Titan IIID Titan IIIE United States Martin Marietta 7 Retired 1974 1977 Titan IIID Titan 34D United States Martin Marietta 15 Retired 1982 1989 Titan 34D Titan IVA United States Martin Marietta Retired 1989 1998 Titan IVA Titan IVB United States Lockheed Martin [75] 21,682[75] 5,761 to GTO
(9,000 with upper stage)432 39 Retired 1997 2005 Titan IVB Tronador 2.0 Argentina CONAE 0 Development[citation needed] Tronador 2.0 Tsyklon-2A Soviet Union Yuzhmash 8 Retired 1967 1969 Tsyklon-2A Tsyklon-2 Soviet Union
UkraineYuzhmash 106 Retired 1969 2006 Tsyklon-2 Tsyklon-3 Soviet Union
UkraineYuzhmash Retired 1977 2009 Tsyklon-3 Tsyklon-4 Ukraine Yuzhmash 0 Development Tsyklon-4 Unha North Korea KCST 100 2 Operational 2006 Unha Vanguard United States Martin 23 11(+1) Retired 1957 1959 Vanguard Vega Europe ESA/ASI 1,500 0 Development
since 1998Vega VLS-1 Brazil AEB 380 [note 14] 2Operational 1997 VLS-1 Volna Russia Makeyev 100 [A] 1(+5)Operational[citation needed] 1995[note 15] Volna Voskhod Soviet Union RSC Energia Retired 1963 1976 Voskhod Vostok-L Soviet Union RSC Energia 4 Retired 1960 1960 Vostok-L Vostok-K Soviet Union RSC Energia Retired 1960 1964 Vostok-K Vostok-2 Soviet Union RSC Energia 45 Retired 1962 1967 Vostok-2 Vostok-2M Soviet Union RSC Energia 93 Retired 1964 1991 Vostok-2M Soyuz/Vostok Soviet Union RSC Energia Retired 1965 1966 Soyuz/Vostok Zenit-2 Soviet Union
UkraineYuzhnoye [76] 13,740[43] 37Retired 1985 2004[77] Zenit-2 Zenit-2M (2SLB) Ukraine Yuzhnoye [76] 13,9201 Operational 2007 Zenit-2M (2SLB) Zenit-3F Ukraine Yuzhnoye[note 16] 1 Operational 2011 Zenit-3F Zenit-3SL Ukraine Yuzhmash
RKK Energia [note 17]6,100 5,250 to GTO €60 million[2] 30 Operational 1999 Zenit-3SL Zenit-3SLB Ukraine Yuzhmash
RKK Energia [note 16]3,750 to GTO 4 Operational 2008 Zenit-3SLB Proposed and design concepts
Main article: List of launch vehicle plansNotes
- ^ A full listing of the Ariane 5 launch history is in its main article.
- ^ Suborbital test in 1969, first orbital launch attempt in 1970
- ^ a b c d e f g h i j k l With 9.5 foot (2.9 metre) fairing
- ^ No flights planned, but 5 unsold heavies could be used.
- ^ Without Buran, and assuming payload providing orbital insertion
- ^ Encyclopedia Astronautica quotes Energia's "flyaway unit cost" at "$764 million in 1985 dollars". However the realistic exchange rate of Soviet currency was drastically different from the official conversion rate which had been set by decree at 0.8 Soviet rubles per US$1. Unofficially one US dollar in 1980s was in terms of purchasing power roughly equivalent to four Soviet rubles.
- ^ a b The US 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.
- ^ Not including two launches made using the H-II/SSB and H-IIS configurations
- ^ Only launch failed to achieve orbit
- ^ Suborbital test flights in 1995, 1997 and 2002, no orbital launches attempted
- ^ The N1 rocket was initially designed for 75mt LEO capacity and launch attempts were made with this version, but there were studies to increase the payload capacity to 90—95 mt, if a liquid-hydrogen upper stage engine could be developed.
- ^ 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). 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.
- ^ Suborbital test flight in 2004, first orbital launch in 2006
- ^ A third rocket exploded before launch
- ^ First orbital launch attempt in 2005
- ^ a b Operated by Land Launch
- ^ Operated by Sea Launch
References
- ^ a b c "Angaga Launch Vehicle Family". Khrunichev. http://www.khrunichev.ru/main.php?id=44.
- ^ a b c d e European Space Directory 2006. Referenced in: Brian Harvey, The Rebirth of the Russian Space Program. p.296.
- ^ a b Семейство ракет-носителей «Ангара», date unknown, Retrieved 2010-08-09.
- ^ a b http://www.russianspaceweb.com/angara7.html
- ^ 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 Gunter, Krebs. "Ariane-1, -2, -3, -4". Gunter's Space Page. http://space.skyrocket.de/doc_lau/ariane.htm. Retrieved 2 August 2011.
- ^ a b "Ariane 5 Users Manual, Issue 4, P. 39 (ISS orbit)" (PDF). Arianespace. Archived from the original on 2007-09-27. http://web.archive.org/web/20070927021638/http://www.arianespace.com/site/documents/Ariane5_users_manual_Issue4.pdf. Retrieved 2007-11-13.
- ^ "Ariane 5 delivers a record performance with two payloads for new Arianespace customers". Arianespace. http://www.arianespace.com/news-mission-update/2011/789.asp. Retrieved 2011-04-11.
- ^ a b c d e f "FAA Semi-Annual Launch Report: Second Half of 2009". Federal Aviation Administration - Office of Commercial Space Transportation. pp. end of document. http://www.faa.gov/about/office_org/headquarters_offices/ast/media/10998.pdf. Retrieved August 18, 2011.
- ^ a b c d e f g h http://space.skyrocket.de/doc_lau/ariane5.htm
- ^ a b c Flight V193 was the seventh Ariane 5 launch of 2009 and used the last of the GS version of the launcher.
- ^ Encyclopedia Astronautica, Athena 1
- ^ a b Lockheed Martin and ATK Announce 2nd Generation Athena Launch Vehicles
- ^ Encyclopedia Astronautica, Athena 2
- ^ a b c d e f g h i j k l m n o p q r s t u v w Gunter, Krebs. "Atlas Centaur". Gunter's Space Page. http://space.skyrocket.de/doc_lau/atlas_centaur.htm. Retrieved 1 August 2011.
- ^ 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 Gunter, Krebs. "Atlas-5". Gunter's Space Page. http://space.skyrocket.de/doc_lau/atlas-5.htm. Retrieved 1 August 2011.
- ^ 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 bb bc bd be bf bg Gunter, Krebs. "Delta". Gunter's Space Page. Archived from the original on 2 August 2011. http://www.webcitation.org/60dqY3Xtj. Retrieved 2 August 2011.
- ^ Wade, Mark. "Delta 0300". Encyclopedia Astronautica. Archived from the original on 2 August 2011. http://www.webcitation.org/60dqp35oP. Retrieved 2 August 2011.
- ^ Wade, Mark. "Delta 0900". Encyclopedia Astronautica. Archived from the original on 2 August 2011. http://www.webcitation.org/60dqt327u. Retrieved 2 August 2011.
- ^ a b Wade, Mark. "Delta 2913". Encyclopedia Astronautica. Archived from the original on 2 August 2011. http://www.webcitation.org/60dt0Zu2u. Retrieved 2 August 2011.
- ^ Wade, Mark. "Delta 4000". Encyclopedia Astronautica. Archived from the original on 2 August 2011. http://www.webcitation.org/60e2WpW6v. Retrieved 2 August 2011.
- ^ Wade, Mark. "Delta 5000". Encyclopedia Astronautica. Archived from the original on 2 August 2011. http://www.webcitation.org/60e2dul4v. Retrieved 2 August 2011.
- ^ a b "Delta Product Sheet, FINAL" (PDF). United Launch Alliance. Archived from the original on 2007-09-28. http://web.archive.org/web/20070928093124/http://www.ulalaunch.com/images/product_sheet/Delta_Product_Sheet_FINAL.pdf. Retrieved 2007-11-14.
- ^ http://www.spaceflightnow.com/news/n1111/10orioneft1/
- ^ a b c d e f Gunter, Krebs. "Delta-4". Gunter's Space Page. Archived from the original on 2 August 2011. http://www.webcitation.org/60e9nhnjT. Retrieved 2 August 2011.
- ^ a b c d e f Space launch report -Delta4
- ^ New communications craft launched for U.S. military, Spaceflight Now, 5 Dec 2009
- ^ Gunter, Krebs. "Dnepr-1". Gunter's Space Page. Archived from the original on 2 August 2011. http://www.webcitation.org/60eARVyOE. Retrieved 2 August 2011.
- ^ a b c d "S.P.Korolev RSC Energia - LAUNCHERS". Energia. http://www.energia.ru/english/energia/launchers/vehicle_energia.html.
- ^ Wade, Mark. "Energia". Encyclopedia Astronautica. http://www.astronautix.com/fam/energia.htm. Retrieved 9 August 2010.
- ^ a b "Projects&Products". IHI Aerospace. http://www.ihi.co.jp/ia/en/product/rocket.html. Retrieved 2011-03-08.
- ^ a b c d e f g h i "Satellite Launch Vehicles". Institute of Space and Astronautical Science (ISAS). http://www.isas.jaxa.jp/e/enterp/rockets/vehicles/index.shtml. Retrieved 4 March 2011.
- ^ a b "Space Exploration Technologies Corporation - Falcon 1". http://www.spacex.com/falcon1.php. Retrieved 2010-10-29.
- ^ a b c "FALCON 9 OVERVIEW". SpaceX. http://www.spacex.com/falcon9.php.
- ^ "Falcon 9 Overview". Space Exploration Technologies. http://spacex.com/falcon9.php. Retrieved 29 Oct 2010.
- ^ a b c "SpaceX Brochure". http://www.spacex.com/downloads/spacex-brochure.pdf. Retrieved 14 June 2011.
- ^ ISRO GSLV Mark I & Mark II, Indian Space Research Organisation, 2008, accessed 2010-12-26.
- ^ Geosynchronous Satellite Launch Vehicle Mark III, ISRO
- ^ "GSLV MK3 (LVM3)". ISRO. 2009. http://knol.google.com/k/indian-space-projects#GSLV_Mk(2D)3_(28)LVM3(29). Retrieved 26 December 2010.
- ^ a b c Gunter, Krebs. "H-2". Gunter's Space Page. http://space.skyrocket.de/doc_lau/h-2.htm. Retrieved 1 August 2011.
- ^ a b c d e f g h i Gunter, Krebs. "H-2A". Gunter's Space Page. http://space.skyrocket.de/doc_lau/h-2a.htm. Retrieved 1 August 2011.
- ^ "Development Plan for Future Mission from HTV System, P. 6 (Table 4 Cargo transfer capabilities)". Jaxa. http://www.senkyo.co.jp/ists2008/pdf/2008-k-64.pdf. Retrieved 28 August 2008.[dead link]
- ^ "H-IIB Launch Vehicle, P. 2". Jaxa. http://www.jaxa.jp/pr/brochure/pdf/01/rocket05.pdf. Retrieved 3 September 2008.
- ^ a b Space lauch report - launch success rates
- ^ 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. http://nissan-heritage-collection.com/NEWS/publicContents/index.php?procType=CATEGORY&catID=14. Retrieved 8 March 2011.
- ^ Long March 1
- ^ 中国大推力火箭技术已被日本大幅超越, 长征三号甲火箭应用氢氧发动机.
- ^ "长征三号甲运载火箭简述". http://news.sina.com.cn/c/2007-09-13/103113882288.shtml. Retrieved 31 October 2011.
- ^ "长征三号甲运载火箭简述". http://news.sina.com.cn/c/2007-09-13/103113882288.shtml. Retrieved 31 October 2011.
- ^ a b "ChangZheng 5 (Long March 5) Launch Vehicle". SinoDefence.com. 2009-02-20. http://www.sinodefence.com/space/launcher/changzheng5.asp. Retrieved 2009-03-06.
- ^ Minotaur I
- ^ "Complex N1-L3". Energia. http://www.energia.ru/en/history/systems/vehicles/vehicle_n1-l3.html.
- ^ Astronautix.com about N1-L3
- ^ S.P.Korolev RSC Energia about N1-L3 components
- ^ Wade, Mark. "N1". Encyclopedia Astronautica. http://www.astronautix.com/lvs/n1.htm. Retrieved 9 August 2010.
- ^ a b "Proton Launch System Mission Planner’s Guide, LKEB-9812-1990". International Launch Services. pp. 2–2. Archived from the original on 2007-10-27. http://web.archive.org/web/20071027045349/http://www.ilslaunch.com/products/proton/protonmpg/protonr6/pmpg_2e.pdf. Retrieved 2007-11-12. "LEO i = 51.6°, H = 200 km circular ... GTO (1800 m/s from GSO) i = 31.0°, Hp = 2100 km, Ha = 35,786 km"
- ^ a b c d "Space Transportation Costs: Trends in Price Per Pound to Orbit 1990-2000" (PDF). Futron. http://www.futron.com/upload/wysiwyg/Resources/Whitepapers/Space_Transportation_Costs_Trends_0902.pdf. Retrieved 2010-05-02.
- ^ Encyclopedia Astronautica - Proton
- ^ a b "PSLV variants capability". ISRO. http://1.bp.blogspot.com/_JRgHKYCaeH4/S-mJE29KQwI/AAAAAAAAAJk/ctRSrE7P72c/s1600/PSLV+variants1.jpg. Retrieved 15 May 2010.
- ^ a b c d e f Gunter, Krebs. "PSLV". Gunter's Space Page. Archived from the original on 2 August 2011. http://www.webcitation.org/60eAq5vzm. Retrieved 2 August 2011.
- ^ Harvey, Brian (2007). "Launchers and engines". The Rebirth of the Russian Space Program (1st ed.). Germany: Springer. ISBN 9780387713540.
- ^ "Rockot Launch Vehicle". Khrunichev. http://www.khrunichev.ru/main.php?id=43.
- ^ Bilstein, Roger E.. "Appendix C: Saturn Family/Mission Data". Stages to Saturn A Technological History of the Apollo/Saturn Launch Vehicles. NASA History Office. http://history.nasa.gov/SP-4206/app-c.htm. Retrieved 7 April 2011.
- ^ a b "Rocket and Space Technology". braeunig. http://www.braeunig.us/space/specs/saturn.htm.
- ^ "SP-4221 The Space Shuttle Decision- Chapter 6: ECONOMICS AND THE SHUTTLE". NASA. http://history.nasa.gov/SP-4221/ch6.htm. Retrieved 2011-01-15.
- ^ Alan Lawrie and Robert Godwin, Saturn, 2005 (paperback, Apogee Books Space Series, 2010), ISBN 1894959191
- ^ John Duncan, Saturn V Flight History (1999), web page (accessed 20 August 2010)
- ^ "Iranian DM: Simorgh to Carry Tolou, Mesbah Satellites into Space". Fars News Agency. 2010-02-03. http://english.farsnews.com/newstext.php?nn=8811141592. Retrieved 2010-02-03.
- ^ http://www.payvand.com/news/10/feb/1025.html
- ^ http://www.nasa.gov/pdf/594163main_2011-SLS_Industry_Day_Final_Public1-1_rev2.pdf
- ^ "The NASA Authorization Act of 2010". United States Senate. July 15, 2010. http://commerce.senate.gov/public/index.cfm?p=Legislation&ContentRecord_id=8d7c1465-f852-4835-ba84-25faf56bbb36&ContentType_id=03ab50f5-55cd-4934-a074-d6928b9dd24c&Group_id=6eaa2a03-6e69-4e43-8597-bb12f4f5aede. Retrieved February 2, 2011.
- ^ "Soyuz-U" launch vehicle State Research and Production Space-Rocket Center "TsSKB-Progress"
- ^ "Soyuz-FG" launch vehicle State Research and Production Space-Rocket Center "TsSKB-Progress"
- ^ [1]
- ^ a b "Taurus II User’s Manual, Rev. 1.3" (PDF). Orbital. April 2010. http://www.orbital.com/NewsInfo/Publications/Taurus_II_Guide.pdf.
- ^ a b "Fact Sheet - TITAN IVB". United States Air Force. https://www.maxwell.af.mil/au/awc/space/factsheets/titan_ivb.htm. Retrieved 2007-11-12.
- ^ a b Space launch report -zenit
- ^ Zenit launch log
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