Dalam penerbangan angkasa, kendaraan peluncur atau roket pembawa adalah roket yang digunakan untuk membawa muatan dari permukaan bumi ke luar angkasa. Sebuah sistem peluncuran termasuk kendaraan peluncur, panggung stage peluncuran dan infrastruktur lainnya. Biasanya muatan payload adalah satelit buatan yang ditempatkan ke orbit, tetapi beberapa spaceflights yang sub-orbital sementara yang lain memungkinkan pesawat ruang angkasa untuk keluar dari orbit Bumi seluruhnya. Sebuah kendaraan peluncuran yang membawa muatan pada lintasan suborbital sering disebut sounding roket.
Peluncuran kendaraan, kendaraan peluncur khususnya orbital, memiliki minimal dua tahap, tetapi kadang-kadang sampai 4.
Jenis kendaraan peluncuran Sunting
Dengan platform peluncuran Sunting
- Darat: Spaceport dan silo rudal tetap (Strela) untuk dikonversi ICBM
- Laut: Platform tetap (San Marco), platform mobile (Sea Launch), kapal selam (Shtil', Volna) untuk dikonversi SLBM
- Udara: Pesawat (Pegasus, Virgin Galactic LauncherOne, Stratolaunch Sistem), balon (ARCASPACE), JP Aerospace Orbital Ascender, proposal permanen pelabuhan ruang angkasa Buoyant
Dengan ukuran Sunting
Ada banyak cara untuk mengklasifikasikan ukuran kendaraan peluncuran. The Komisi Agustinus yang diciptakan untuk meninjau rencana untuk mengganti Space Shuttle, menggunakan skema klasifikasi berikut:
- Roket sonda tidak dapat mencapai orbit dan hanya mampu spaceflight sub-orbital.
- Kendaraan peluncur angkut ringan mampu mengangkut hingga 2.000 kg (£ 4400) dari muatan ke orbit bumi rendah (LEO).
- Kendaraan peluncur angkut medium mampu mengangkut antara 2.000 sampai 20.000 kg (4.400 sampai £ 44.000) dari muatan ke LEO.
- Kendaraan peluncur angkut berat mampu mengangkut antara 20.000 sampai 50.000 kg (44.000 sampai £ 110.200) dari muatan ke LEO.
- Kendaraan peluncur angkut superberat mampu mengangkut lebih dari 50.000 kg (110.200 £ +) dari muatan ke LEO.
Perakitan Sunting
Setiap tahap roket individu umumnya dikumpulkan di lokasi pabrik dan dikirim ke lokasi peluncuran; jangka waktu perakitan kendaraan mengacu pada penggabungan tahap roket dengan muatan pesawat ruang angkasa dalam satu kendaraan perakitan yang dikenal sebagai kendaraan ruang angkasa.
Kendaraan tahap tunggal (seperti sounding roket), dan kendaraan multi tahap mulai yang lebih kecil dari berbagai ukuran, biasanya dapat dirakit secara vertikal, langsung di landasan peluncuran dengan mengangkat setiap tahap pesawat ruang angkasa dan secara berurutan di tempat dengan cara diderek.
Perbandingan sistem peluncur orbital Sunting
Keterangan singkatan orbit dalam tabel:
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Legend for launch system status in below table: [under development] — [retired] — [operational]
Vehicle | Origin | Manufacturer | Mass to LEO (kg) | Mass to other orbits (kg) | Cost (Mil US$) | Cost/kg (LEO) (US$) | Cost/kg (GTO) (US$) | Launches | Status | First flight | Last flight | Vehicle |
---|---|---|---|---|---|---|---|---|---|---|---|---|
Angara 1.1 | Rusia | Khrunichev | 0 | Development | Angara 1.1 | |||||||
Angara 1.2 | Rusia | Khrunichev | 3.800 | 0 | Development | Angara 1.2 | ||||||
Angara A3 | Rusia | Khrunichev | 14.600 | 2.400–3,600 to GTO | €50 (US$70) | 0 | Development | Angara A3 | ||||
Angara A5 | Rusia | Khrunichev | 24.500 (63°) | 0 | Development | Angara A5 | ||||||
Angara A7 | Rusia | Khrunichev | 41.000 | 0 | Development | Angara A7 | ||||||
Ariane 1 | Europe | Aérospatiale | 1.400 | 1.830 to GTO | 11 | Retired | 1979 | 1986 | Ariane 1 | |||
Ariane 2 | Europe | Aérospatiale | 2.270 to GTO | 6 | Retired | 1986 | 1989 | Ariane 2 | ||||
Ariane 3 | Europe | Aérospatiale | 2.650 to GTO | 11 | Retired | 1984 | 1989 | Ariane 3 | ||||
Ariane 4 40 | Europe | Aérospatiale | 4.600 | 1,900 to GTO | 2.740 to SSO3 | Retired | 1990 | 1993 | Ariane 4 40 | |||
Ariane 4 40 H10+ | Europe | Aérospatiale | 2.020 to GTO | 1 | Retired | 1995 | 1995 | Ariane 4 40 H10+ | ||||
Ariane 4 40 H10-3 | Europe | Aérospatiale | 2.105 to GTO | 3 | Retired | 1995 | 1999 | Ariane 4 40 H10-3 | ||||
Ariane 4 42L | Europe | Aérospatiale | 7.000 | 3,200 to GTO | 4.500 to SSO1 | Retired | 1993 | 1993 | Ariane 4 42L | |||
Ariane 4 42L H10+ | Europe | Aérospatiale | 7.000 | 3.350 to GTO | 1 | Retired | 1994 | 1994 | Ariane 4 42L H10+ | |||
Ariane 4 42L H10-3 | Europe | Aérospatiale | 7.000 | 3.480 to GTO | 11 | Retired | 1995 | 2002 | Ariane 4 42L H10-3 | |||
Ariane 4 42P | Europe | Aérospatiale | 6.000 | 2,600 to GTO | 3,400 to SSO2 | Retired | 1990 | 1992 | Ariane 4 42P | |||
Ariane 4 42P H10+ | Europe | Aérospatiale | 2.740 to GTO | 4 | Retired | 1992 | 1994 | Ariane 4 42P H10+ | ||||
Ariane 4 42P H10-3 | Europe | Aérospatiale | 2.930 to GTO | 9 | Retired | 1994 | 2002 | Ariane 4 42P H10-3 | ||||
Ariane 4 44L | Europe | Aérospatiale | 7.000 | 4,200 to GTO | 6,000 to SSO11 | Retired | 1989 | 1992 | Ariane 4 44L | |||
Ariane 4 44L H10+ | Europe | Aérospatiale | 7.000 | 4.460 to GTO | 5 | Retired | 1992 | 1994 | Ariane 4 44L H10+ | |||
Ariane 4 44L H10-3 | Europe | Aérospatiale | 7.000 | 4.720 to GTO | 24 | Retired | 1995 | 2003 | Ariane 4 44L H10-3 | |||
Ariane 4 44LP | Europe | Aérospatiale | 7.000 | 3,700 to GTO | 5,000 to SSO7 | Retired | 1988 | 1993 | Ariane 4 44LP | |||
Ariane 4 44LP H10+ | Europe | Aérospatiale | 7.000 | 4.030 to GTO | 6 | Retired | 1992 | 1995 | Ariane 4 44LP H10+ | |||
Ariane 4 44LP H10-3 | Europe | Aérospatiale | 7.000 | 4.220 to GTO | 13 | Retired | 1995 | 2001 | Ariane 4 44LP H10-3 | |||
Ariane 4 44P | Europe | Aérospatiale | 6.500 | 3,000 to GTO | 4,100 to SSO2 | Retired | 1991 | 1991 | Ariane 4 44P | |||
Ariane 4 44P H10-3 | Europe | Aérospatiale | 3.465 to GTO | 9 | Retired | 1995 | 2001 | Ariane 4 44P H10-3 | ||||
Ariane 5ECA | Europe | EADS Astrium | 21.000 | 10.050 to GTO | 220 | 10.476 | Operational | 2002 | ||||
Ariane 5ME | Europe | EADS Astrium | 11.500 to GTO | 0 | Development | Ariane 5ME | ||||||
Ariane 5ES | Europe | EADS Astrium | 21.000 | 8.000 to GTO | 220 | 10,476 | 2 | Operational | 2008 | Ariane 5ES | ||
Ariane 5G | Europe | EADS Astrium | 18.000 | 6.900 | 16 | Retired | 1996 | 2003 | Ariane 5G | |||
Ariane 5G+ | Europe | EADS Astrium | [butuh rujukan] | 18.0007.100 to GTO | 3 | Retired | 2004 | 2004 | Ariane 5G+ | |||
Ariane 5GS | Europe | EADS Astrium | [butuh rujukan] | 18.0006.600 to GTO | 6 | Retired | 2005 | 2009 | Ariane 5GS | |||
Ariane 6 | Europe | EADS Astrium | 6.500 to GTO | 93 | 0 | Development | Ariane 6 | |||||
ASLV | India | ISRO | 1987 | 1994 | ASLV | |||||||
Athena I | Amerika Serikat | Lockheed Martin | 4 | Retired | 1995 | 2001 | Athena I | |||||
Athena Ic | Amerika Serikat | ATK Lockheed Martin | 0 | Development | Athena Ic | |||||||
Athena II | Amerika Serikat | Lockheed Martin | [butuh rujukan] | 2.0653 | Retired[butuh rujukan] | 1998 | 1999 | Athena II | ||||
Athena IIc | Amerika Serikat | ATK Lockheed Martin | 0 | Development | Athena IIc | |||||||
Atlas-Centaur | Amerika Serikat | Lockheed | [butuh rujukan] | 8.618[butuh rujukan] | 3.833 to GTO148 | Retired | 1962 | 1983 | Atlas-Centaur | |||
Atlas G | Amerika Serikat | Lockheed | 5.900 | 1,179 to HCO | 2.222 to GTO7 | Retired | 1984 | 1989 | Atlas G | |||
Atlas H/MSD | Amerika Serikat | Lockheed | 5 | Retired | 1983 | 1987 | Atlas H/MSD | |||||
Atlas I | Amerika Serikat | Lockheed Martin | 5.900 | 2.340 | 11 | Retired | 1990 | 1997 | Atlas I | |||
Atlas II | Amerika Serikat | Lockheed Martin | 6.780 | 2,000 to HCO | 2.810 to GTO10 | Retired | 1991 | 1998 | Atlas II | |||
Atlas IIA | Amerika Serikat | Lockheed Martin | 7.316 | 2,160 to HCO | 3.180 to GTO23 | Retired | 1992 | 2002 | Atlas IIA | |||
Atlas IIAS | Amerika Serikat | Lockheed Martin | 8.618 | 2,680 to HCO | 3.833 to GTO30 | Retired | 1993 | 2004 | Atlas IIAS | |||
Atlas IIIA | Amerika Serikat | Lockheed Martin | 8.686 | 2,970 to HCO | 4.060 to GTO2 | Retired | 2000 | 2004 | Atlas IIIA | |||
Atlas IIIB/DEC | Amerika Serikat | Lockheed Martin | 10.759 | 4.609 to GTO | 1 | Retired | 2002 | 2002 | Atlas IIIB/DEC | |||
Atlas IIIB/SEC | Amerika Serikat | Lockheed Martin | 4.193 to GTO | 3 | Retired | 2003 | 2005 | Atlas IIIB/SEC | ||||
Atlas V 401 | Amerika Serikat | United Launch Alliance | 9.050 | 4,950 to GTO | 6,670 to SSO125 | 13,812 | 18 | Operational | 2002 | Atlas V 401 | ||
Atlas V 411 | Amerika Serikat | United Launch Alliance | 9.050 | 6,075 to GTO | 8,495 to SSO3 | Operational | 2006 | Atlas V 411 | ||||
Atlas V 421 | Amerika Serikat | United Launch Alliance | 9.050 | 7,000 to GTO | 9,050 to SSO3 | Operational | 2007 | Atlas V 421 | ||||
Atlas V 431 | Amerika Serikat | United Launch Alliance | 9.050 | 7,800 to GTO | 9,050 to SSO2 | Operational | 2005 | Atlas V 431 | ||||
Atlas V 501 | Amerika Serikat | United Launch Alliance | 8.250 | 3,970 to GTO 1,500 to GEO | 5,945 to SSO4 | Operational | 2010 | Atlas V 501 | ||||
Atlas V 511 | Amerika Serikat | United Launch Alliance | 10.950 | 5,370 to GTO 1,750 to GEO | 7,820 to SSO0 | Operational | Atlas V 511 | |||||
Atlas V 521 | Amerika Serikat | United Launch Alliance | 13.300 | 6,485 to GTO 2,760 to GEO | 9,585 to SSO2 | Operational | 2003 | Atlas V 521 | ||||
Atlas V 531 | Amerika Serikat | United Launch Alliance | 15.300 | 7,425 to GTO 3,250 to GEO | 11,160 to SSO2 | Operational | 2010 | Atlas V 531 | ||||
Atlas V 541 | Amerika Serikat | United Launch Alliance | 17.100 | 8,240 to GTO 3,730 to GEO | 12,435 to SSO223 (2013) | 27,063 | 1 | Operational | Atlas V 541 | |||
Atlas V 551 | Amerika Serikat | United Launch Alliance | 18.500 | 8,700 to GTO 3,960 to GEO | 12,435 to SSO4 | Operational | 2006 | Atlas V 551 | ||||
Black Arrow | Britania Raya | RAE | 73 | 2 | Retired | 1969 | 1971 | Black Arrow | ||||
Commercial Titan III | Amerika Serikat | Martin Marietta | 4 | Retired | 1990 | 1992 | Commercial Titan III | |||||
Delta 0300 | Amerika Serikat | McDonnell Douglas | [butuh rujukan] | 700[butuh rujukan] | 370 to SSO3 | Retired | 1972 | 1973 | Delta 0300 | |||
Delta 0900 | Amerika Serikat | McDonnell Douglas | 1.300 | 818 to SSO | 2 | Retired | 1972 | 1972 | Delta 0900 | |||
Delta 1410 | Amerika Serikat | McDonnell Douglas | 1 | Retired | 1975 | 1975 | Delta 1410 | |||||
Delta 1604 | Amerika Serikat | McDonnell Douglas | 2 | Retired | 1972 | 1973 | Delta 1604 | |||||
Delta 1900 | Amerika Serikat | McDonnell Douglas | 1.800 | 1 | Retired | 1973 | 1973 | Delta 1900 | ||||
Delta 1910 | Amerika Serikat | McDonnell Douglas | 1 | Retired | 1975 | 1975 | Delta 1910 | |||||
Delta 1913 | Amerika Serikat | McDonnell Douglas | 1 | Retired | 1973 | 1973 | Delta 1913 | |||||
Delta 1914 | Amerika Serikat | McDonnell Douglas | 2 | Retired | 1972 | 1973 | Delta 1914 | |||||
Delta 2310 | Amerika Serikat | McDonnell Douglas | 3 | Retired | 1974 | 1981 | Delta 2310 | |||||
Delta 2313 | Amerika Serikat | McDonnell Douglas | 3 | Retired | 1974 | 1977 | Delta 2313 | |||||
Delta 2910 | Amerika Serikat | McDonnell Douglas | 1.887 | 6 | Retired | 1975 | 1978 | Delta 2910 | ||||
Delta 2913 | Amerika Serikat | McDonnell Douglas | 2.000 | 700 to GTO | 6 | Retired | 1975 | 1976 | Delta 2913 | |||
Delta 2914 | Amerika Serikat | McDonnell Douglas | 724 to GTO | 30 | Retired | 1974 | 1979 | Delta 2914 | ||||
Delta 3910 | Amerika Serikat | McDonnell Douglas | 2.494 | 1.154 to GTO with PAM-D | 10 | Retired | 1980 | 1988 | Delta 3910 | |||
Delta 3913 | Amerika Serikat | McDonnell Douglas | 1 | Retired | 1981 | 1981 | Delta 3913 | |||||
Delta 3914 | Amerika Serikat | McDonnell Douglas | 954 to GTO | 13 | Retired | 1975 | 1987 | Delta 3914 | ||||
Delta 3920 | Amerika Serikat | McDonnell Douglas | 3.452 | 1.284 to GTO with PAM-D | 10 | Retired | 1982 | 1989 | Delta 3920 | |||
Delta 3924 | Amerika Serikat | McDonnell Douglas | 1.104 to GTO | 4 | Retired | 1982 | 1984 | Delta 3924 | ||||
Delta 4925 | Amerika Serikat | McDonnell Douglas | 3.400 | 1.312 to GTO | 2 | Retired | 1989 | 1990 | Delta 4925 | |||
Delta 5920 | Amerika Serikat | McDonnell Douglas | 3.848 | 1 | Retired | 1989 | 1989 | Delta 5920 | ||||
Delta II 6920 | Amerika Serikat | McDonnell Douglas | 3.983 | 3 | Retired | 1990 | 1992 | Delta II 6920 | ||||
Delta II 6925 | Amerika Serikat | McDonnell Douglas | 1.447 to GTO | 14 | Retired | 1989 | 1992 | Delta II 6925 | ||||
Delta II 7320 | Amerika Serikat | United Launch Alliance | 2.865 | 1.651 to SSO | 10 | Retired | 1999 | 2011 | Delta II 7320 | |||
Delta II 7326 | Amerika Serikat | Boeing IDS | 636 to TLI 629 to HCO | 934 to GTO3 | Retired | 1998[butuh rujukan] | Delta II 7326 | |||||
Delta II 7420 | Amerika Serikat | United Launch Alliance | 3.185 | 1.966 to SSO | 13 | Retired | 1998 | 2010 | Delta II 7420 | |||
Delta II 7425 | Amerika Serikat | Boeing IDS | 804 to HCO | 1.100 to GTO4 | Retired | 1998 | 2002 | Delta II 7425 | ||||
Delta II 7426 | Amerika Serikat | Boeing IDS | 734 to TLI 711 to HCO | 1.058 to GTO1 | Retired | 1999 | 1999 | Delta II 7426 | ||||
Delta II 7920 | Amerika Serikat | United Launch Alliance | 5.030 | 3.123 to SSO | 27 | Operational | 1998 | 2011 | Delta II 7920 | |||
Delta II 7925 | Amerika Serikat | Boeing IDS | 1,177 to TLI 1,265 to HCO | 1.819 to GTO69 | Retired | 1990 | 2009 | Delta II 7925 | ||||
Delta II-H 7920H | Amerika Serikat | United Launch Alliance | 6.097 | 3 | Retired | 2003 | 2011 | Delta II-H 7920H | ||||
Delta II-H 7925H | Amerika Serikat | United Launch Alliance | 1,508 to HCO | 2.171 to GTO3 | Operational [butuh rujukan] | 2003 | 2007 | Delta II-H 7925H | ||||
Delta III 8930 | Amerika Serikat | Boeing IDS | 8.292 | 3.810 to GTO | 3 | Retired | 1998 | 2000 | Delta III 8930 | |||
Delta IV-H | Amerika Serikat | United Launch Alliance | 22.950 | 12.980 to GTO | 300(€220) | [butuh rujukan] | 13.0725 | Operational | 2004 | Delta IV-H | ||
Delta IV-M | Amerika Serikat | Boeing IDS | 8.120 | 2,722 to HCO | 4.210 to GTO3 | Retired | 2003 | 2006 | Delta IV-M | |||
Delta IV-M+(4,2) | Amerika Serikat | United Launch Alliance | 11.750 | 5.740 to GTO | 8 | Operational | 2002 | Delta IV-M+(4,2) | ||||
Delta IV-M+(5,2) | Amerika Serikat | United Launch Alliance | 10.250 | 4.590 to GTO | 0 | Operational | Delta IV-M+(5,2) | |||||
Delta IV-M+(5,4) | Amerika Serikat | United Launch Alliance | 13.500 | 6.470 to GTO | 1 | Operational | 2009 | Delta IV-M+(5,4) | ||||
Diamant | Prancis | SEREB | 12 | Retired | 1965 | 1975 | Diamant | |||||
Dnepr-1 | Ukraina | Yuzhmash | 3.700 | 14(€10) | [butuh rujukan] | 3.78416 | Operational | 1999 | Dnepr-1 | |||
Energia | Uni Soviet | NPO Energia | 100.000 | 32,000 to TLI | 20.000 to GTO240 | 1 | Retired | 1987 | 1987 | Energia | ||
Energia-Buran | Uni Soviet | NPO Energia (Launcher) NPO Molniya (Orbiter) | 1 | Retired | 1988 | 1988 | Energia-Buran | |||||
Epsilon | Jepang | IHI Aerospace | 1.200 | ¥3.8B (US$38) | 31.667 | 1 | Operational | 2013 | Epsilon | |||
Falcon 1 | Amerika Serikat | SpaceX | [butuh rujukan] | 670[butuh rujukan] | 75 | Retired | 2006 | 2009 | Falcon 1 | |||
Falcon 1e | Amerika Serikat | SpaceX | [butuh rujukan] | 1.01010,9 | [butuh rujukan] | 10.7920 | Retired | Falcon 1e | ||||
Falcon 9 v1.0 | Amerika Serikat | SpaceX | 10.450 | 4.680 to GTO | 56 | [butuh rujukan] | 5.3595 | Retired | 2010 | 2013 | Falcon 9 v1.0 | |
Falcon 9 v1.1 | Amerika Serikat | SpaceX | 16.625 | 5.760 to GTO | 56 | 4.109 | 1 | Operational | 2013 | Falcon 9 v1.1 | ||
Falcon Heavy | Amerika Serikat | SpaceX | 53.000 | 16.000 to TLI | 12.000 to GTO83–128 | 2.200 | 0 | Development | Falcon Heavy | |||
GSLV Mk.I(a) | India | ISRO | Retired | 2001 | 2001 | GSLV Mk.I(a) | ||||||
GSLV Mk.I(b) | India | ISRO | Retired | 2004 | 2007[butuh rujukan] | GSLV Mk.I(b) | ||||||
GSLV Mk.I(c) | India | ISRO | [butuh rujukan] | 1Operational | 2010 | GSLV Mk.I(c) | ||||||
GSLV Mk.II | India | ISRO | 2.500 | Operational | 2010 | GSLV Mk.II | ||||||
GSLV Mk.III | India | ISRO | [butuh rujukan] | 10.0005,000 | 0 | Development | GSLV Mk.III | |||||
H-I | Jepang Amerika Serikat | Mitsubishi Heavy Industries | [butuh rujukan] | 3.200[butuh rujukan] | 1.100 to GTO9 | Retired | 1986 | 1992 | H-I | |||
H-II | Jepang | Mitsubishi Heavy Industries | 5 | Retired | 1994 | 1998 | H-II | |||||
H-IIA 202 | Jepang | Mitsubishi Heavy Industries | 10.000 | 3.800 to GTO | 9 | Operational | 2001 | H-IIA 202 | ||||
H-IIA 204 | Jepang | Mitsubishi Heavy Industries | 5.800 to GTO | 1 | Operational | 2006 | 2006 | H-IIA 204 | ||||
H-IIA 2022 | Jepang | Mitsubishi Heavy Industries | 4.200 | 3 | Retired | 2005 | 2007 | H-IIA 2022 | ||||
H-IIA 2024 | Jepang | Mitsubishi Heavy Industries | 7 | Retired | 2002 | 2008 | H-IIA 2024 | |||||
H-IIB 304 | Jepang | Mitsubishi Heavy Industries | 16.500 | 8.000 | 2 | Operational | 2009 | H-IIB 304 | ||||
H-II/SSB | Jepang | Mitsubishi Heavy Industries | 1 | Retired | 1995 | 1995 | H-II/SSB | |||||
H-IIS | Jepang | Mitsubishi Heavy Industries | 1 | Retired | 1999 | 1999 | H-IIS | |||||
J-I | Jepang | IHI Corporation Nissan Motors | 0(+1) | Retired | 1996 | 1996 | J-I | |||||
Kaituozhe-1 | Tiongkok | CALT | 2 | Operational | 2002 | 2003[butuh rujukan] | Kaituozhe-1 | |||||
Kosmos-3M | Uni Soviet Rusia | NPO Polyot | 1.500 | €12 million | [butuh rujukan] | 442Retired | 1967 | 2010[butuh rujukan] | Kosmos-3M | |||
Lambda 4S | Jepang | Nissan Motors | 26 | 5 | Retired | 1966 | 1970[butuh rujukan] | Lambda 4S | ||||
Long March 1 | Tiongkok | CALT | [butuh rujukan] | 3003 | Retired | 1969 | 1971[butuh rujukan] | Long March 1 | ||||
Long March 1D | Tiongkok | CALT | 0(+3) | Operational[butuh rujukan] | 1995 | 2002 | Long March 1D | |||||
Long March 2A | Tiongkok | CALT | 1 | Retired | 1974 | 1974[butuh rujukan] | Long March 2A | |||||
Long March 2C | Tiongkok | CALT | 32 | Operational | 1975[butuh rujukan] | Long March 2C | ||||||
Long March 2D | Tiongkok | CALT | 14 | Operational | 1992[butuh rujukan] | Long March 2D | ||||||
Long March 2E | Tiongkok | CALT | [butuh rujukan] | 7Retired | 1990 | 1995[butuh rujukan] | Long March 2E | |||||
Long March 2F | Tiongkok | CALT | 7 | Operational | 1999[butuh rujukan] | Long March 2F | ||||||
Long March 2F/G | Tiongkok | CALT | 1 | Operational | 2011 | Long March 2F/G | ||||||
Long March 3 | Tiongkok | CALT | 14 | Retired | 1984 | Long March 3 | ||||||
Long March 3A | Tiongkok | CALT | 2.650 to GTO | [butuh rujukan] | 23Operational | 1994 | Long March 3A | |||||
Long March 3B | Tiongkok | CALT | 11,200Templat:Source need translation | [butuh rujukan] | 10Operational | 1996 | Long March 3B | |||||
Long March 3B/E | Tiongkok | CALT | 5,500 to GTO | Operational | 2007[butuh rujukan] | Long March 3B/E | ||||||
Long March 3B(A) | Tiongkok | CALT | 0 | Development[butuh rujukan] | Long March 3B(A) | |||||||
Long March 3C | Tiongkok | CALT | 3.700 | [butuh rujukan] | 8Operational | 2008 | Long March 3C | |||||
Long March 4A | Tiongkok | CALT | [butuh rujukan] | 2Retired | 1988 | 1990[butuh rujukan] | Long March 4A | |||||
Long March 4B | Tiongkok | CALT | 4.200 | 18 | Operational | 1999 | Long March 4B | |||||
Long March 4C | Tiongkok | CALT | Operational | 2007[butuh rujukan] | Long March 4C | |||||||
Long March 5 | Tiongkok | CALT | 25.000 | 14.000 to GTO | 0 | Development[butuh rujukan] | Long March 5 | |||||
Long March 6 | Tiongkok | CALT | 0 | Development[butuh rujukan] since 2009 | Long March 6 | |||||||
Long March 7 | Tiongkok | CALT | 0 | Development since 2009[butuh rujukan] | Long March 7 | |||||||
Long March 9 | Tiongkok | CALT | 130.000 | 0 | Development | Long March 9 | ||||||
M-V | Jepang | Nissan Motors (-2000) IHI AEROSPACE (-2006) | 1.800 - 1,850 | 7 | Retired | 1997 | 2006 | M-V | ||||
Minotaur I | Amerika Serikat | Orbital | 580 | 10 | Operational | 2000 | 2011 | Minotaur I | ||||
Minotaur IV | Amerika Serikat | Orbital | 3(+2) | Operational | 2010 | 2011 | Minotaur IV | |||||
Minotaur V | Amerika Serikat | Orbital | 447 to TLI | 640 to GTO1 | Operational | 2013 | Minotaur V | |||||
Molniya | Uni Soviet | RSC Energia | 24 | Retired | 1960 | 1965 | Molniya | |||||
Molniya-M | Uni Soviet Rusia | RSC Energia | 275 | Retired | 1964 | 2010 | Molniya-M | |||||
Mu-3C | Jepang | Nissan Motors | 195 | 4 | Retired | 1974 | 1979 | Mu-3C | ||||
Mu-3H | Jepang | Nissan Motors | 300 | 3 | Retired | 1977 | 1978 | Mu-3H | ||||
Mu-3S | Jepang | Nissan Motors | 300 | 4 | Retired | 1980 | 1984[butuh rujukan] | Mu-3S | ||||
Mu-3SII | Jepang | Nissan Motors | 770 | 8 | Retired | 1985 | 1995 | Mu-3SII | ||||
Mu-4S | Jepang | Nissan Motors | 180 | 4 | Retired | 1971 | 1972 | Mu-4S | ||||
N1 | Uni Soviet | NPO Energia | 95.000 | 4 | Retired | 1969 | 1972 | N1 | ||||
N-I | Jepang Amerika Serikat | Mitsubishi Heavy Industries | Retired | 1975 | 1982[butuh rujukan] | N-I | ||||||
N-II | Jepang Amerika Serikat | Mitsubishi Heavy Industries | 8 | Retired | 1981 | 1987[butuh rujukan] | N-II | |||||
Naro-1 | Korea Selatan Rusia | KARI/Khrunichev | 3 | Retired | 2009 | 2013 | Naro-1 | |||||
Paektusan | North Korea | KCST | Retired | 1998 | 1998 | |||||||
Pegasus | Amerika Serikat | Orbital | 443 | 41 | Operational | 1990 | 2012 | Pegasus | ||||
Pegasus II | Amerika Serikat | Orbital | 6.120 | 2.000 to GTO | Development | Pegasus II | ||||||
Polyot | Uni Soviet | RSC Energia | 1.400 | Retired | 1963 | 1964[butuh rujukan] | Polyot | |||||
Proton-K | Uni Soviet Rusia | Khrunichev | [butuh rujukan] | 19.760[butuh rujukan] to GTO | 4.930311 | Retired | 1965 | 2012[butuh rujukan] | Proton-K | |||
Proton-M | Uni Soviet Rusia | Khrunichev | 21.600 | 6.150 to GTO | 85 | 4.302 | 61 | Operational | 2001[butuh rujukan] | Proton-M | ||
PSLV | India | ISRO | 3.200 | 1,050 to GTO | 1.600 to SSO11 | Operational | 1993[butuh rujukan] | PSLV | ||||
PSLV-CA | India | ISRO | 2.800 | 1.100 to SSO | 7 | Operational | 2007 | PSLV-CA | ||||
PSLV-XL | India | ISRO | 3.800 | 1,300 to GTO | 1,750 to SSO3 | Operational | 2008 | PSLV-XL | ||||
PSLV-HP | India | ISRO | 4.000 | 1,440 to GTO | 1,900 to SSO0 | Development | PSLV-HP | |||||
Rokot | Rusia | Khrunichev | 1.950 | 14 | [butuh rujukan] | 7.17914 | Operational | 1990 | ||||
Safir | Iran | Iranian Space Agency | 3 | Operational | 2008 | 2012[butuh rujukan] | Safir | |||||
Saturn I | Amerika Serikat | Chrysler (S-I) Douglas (S-IV) | 10 | Retired | 1961 | 1965 | Saturn I | |||||
Saturn IB | Amerika Serikat | Chrysler (S-IB) Douglas (S-IVB) | [butuh rujukan] | 20.4129 | Retired | 1966 | 1975 | Saturn IB | ||||
Saturn V | Amerika Serikat | Boeing (S-IC) North American (S-II) Douglas (S-IVB) | 118.000 | 47.000 to TLI | 185 (126.394 billion in 2023) | [butuh rujukan] | 9,91513 | Retired | 1967 | 1973 | Saturn V | |
Scout | Amerika Serikat | US Air Force/NASA | 150 | 125 | Retired | 1961 | 1994 | Scout | ||||
Shavit | Israel | IAE | 160 | 15 | 9 | Operational | 1988 | 2010 | Shavit | |||
Shtil' | Rusia | Makeyev | 160 - 430 | Operational | 1998 | 2006[butuh rujukan] | Shtil' | |||||
Simorgh | Iran | Iranian Space Agency | 60-100 | 0 | Simorgh | |||||||
SLS Block 1 | Amerika Serikat | Alliant Techsystems (SRBs) Boeing (proposed) | 70.000 | 0 | Development | SLS Block 1 | ||||||
SLS Block 2 | Amerika Serikat | Alliant Techsystems (SRBs) Boeing (proposed) | 130.000 | 0 | Development | SLS Block 2 | ||||||
SLV | India | ISRO | [butuh rujukan] | 40[butuh rujukan] | 41979 | 1983[butuh rujukan] | SLV | |||||
Soyuz | Uni Soviet | RSC Energia | 6.450 | 30 | Retired | 1966 | 1975 | Soyuz | ||||
Soyuz-L | Uni Soviet | RSC Energia | 5.500 | 3 | Retired | 1970 | 1971 | Soyuz-L | ||||
Soyuz-M | Uni Soviet | RSC Energia | 6.600 | 8 | Retired | 1971 | 1976 | Soyuz-M | ||||
Soyuz-U | Uni Soviet Rusia | TsSKB-Progress | Plesetsk) 6590-6950 from Baikonour | 6.200–6,700 kg from 727 | Operational | 1973 | Soyuz-U | |||||
Soyuz-U2 | Uni Soviet Rusia | TsSKB-Progress | 92 | Retired | 1982 | 1995 | Soyuz-U2 | |||||
Soyuz-FG | Rusia | TsSKB-Progress | 6.790–7130 kg | 29 | Operational | 2001 | Soyuz-FG | |||||
Soyuz-2.1a | Rusia | TsSKB-Progress | 7(+1) | Operational | 2004 | Soyuz-2.1a | ||||||
Soyuz-2.1b | Rusia | TsSKB-Progress | 4 | Operational | 2011 | Soyuz-2.1b | ||||||
Soyuz-2.1v | Rusia | TsSKB-Progress | 2.850 | 0 | Development | Soyuz-2.1v | ||||||
Space Shuttle | Amerika Serikat | Alliant Techsystems (SRBs) Martin Marietta (ET) Rockwell International (Orbiter) | 24.400 | 300 | 10.416 | 135 | Retired | 1981 | 2011 | Space Shuttle | ||
Sputnik 8K71PS | Uni Soviet | RSC Energia | 500 | 2 | Retired | 1957 | 1957 | Sputnik 8K71PS | ||||
Sputnik 8A91 | Uni Soviet | RSC Energia | 1.327 | 2 | Retired | 1958 | 1958 | Sputnik 8A91 | ||||
Start-1 | Rusia | MITT | [butuh rujukan] | 532[butuh rujukan] | 167 to SSO[butuh rujukan] | 7Operational | 1993 | 2006[butuh rujukan] | Start-1 | |||
StratoLaunch | Amerika Serikat | Stratolaunch Systems | 6.100 | Development | 2016 | StratoLaunch | ||||||
Strela | Rusia | Khrunichev | 1.700 | €5 million. | Operational[butuh rujukan] | 2003 | 2003 | Strela | ||||
Super Haas | Rumania | ARCA | 2.600 | 0 | Development | Super Haas | ||||||
Taurus | Amerika Serikat | Orbital | [butuh rujukan] | 1.320[butuh rujukan] | 9Operational | 1994 | 2011[butuh rujukan] | Taurus | ||||
Antares | Amerika Serikat | Orbital | 6.000 | 1.900 to GTO | 2 | Operational | 2013 | 2013 | Antares | |||
Titan II GLV | Amerika Serikat | Martin Marietta | 11(+1) | Retired | 1964 | 1966 | Titan II GLV | |||||
Titan II(23)G | Amerika Serikat | Martin Marietta | 13 | Retired | 1988 | 2003 | Titan II(23)G | |||||
Titan IIIA | Amerika Serikat | Martin Marietta | Retired | 1964 | 1965 | Titan IIIA | ||||||
Titan IIIB | Amerika Serikat | Martin Marietta | 70 | Retired | 1966 | 1987 | Titan IIIB | |||||
Titan IIIC | Amerika Serikat | Martin Marietta | 36 | Retired | 1965 | 1982 | Titan IIIC | |||||
Titan IIID | Amerika Serikat | Martin Marietta | 22 | Retired | 1971 | 1982 | Titan IIID | |||||
Titan IIIE | Amerika Serikat | Martin Marietta | 7 | Retired | 1974 | 1977 | Titan IIID | |||||
Titan 34D | Amerika Serikat | Martin Marietta | 15 | Retired | 1982 | 1989 | Titan 34D | |||||
Titan IVA | Amerika Serikat | Martin Marietta | 22 | Retired | 1989 | 1998 | Titan IVA | |||||
Titan IVB | Amerika Serikat | Lockheed Martin | 21.682 | (9,000 with upper stage) | 5.761 to GTO 432 | [butuh rujukan] | 13.83617 | Retired | 1997 | 2005 | Titan IVB | |
Tronador II | Argentina | CONAE | 0 | Development | Tronador 2.0 | |||||||
Tsyklon-2A | Uni Soviet | Yuzhmash | 8 | Retired | 1967 | 1969 | Tsyklon-2A | |||||
Tsyklon-2 | Uni Soviet Ukraina | Yuzhmash | 106 | Retired | 1969 | 2006 | Tsyklon-2 | |||||
Tsyklon-3 | Uni Soviet Ukraina | Yuzhmash | 122 | Retired | 1977 | 2009 | Tsyklon-3 | |||||
Tsyklon-4 | Ukraina | Yuzhmash | 5.500 | 1.700 to GTO | 0 | Development | Tsyklon-4 | |||||
Unha | North Korea | KCST | [butuh rujukan] | 100[butuh rujukan] | 2Operational[butuh rujukan] | 2006 | 2009[butuh rujukan] | Unha | ||||
Vanguard | Amerika Serikat | Martin | [butuh rujukan] | 2311(+1) | Retired | 1957 | 1959 | Vanguard | ||||
Vega | Europe | ESA/ASI | 1.500 | 23,5 | [butuh rujukan] | 15.6002 | Operational | 2012 | Vega | |||
VLS-1 | Brasil | AEB, INPE | 380 | 2 | Operational | 1997 | 2003 | VLS-1 | ||||
Volna | Rusia | Makeyev | 100 | [A] | 1(+5)Operational[butuh rujukan] | 1995 | 2005 | Volna | ||||
Voskhod | Uni Soviet | RSC Energia | 306 | Retired | 1963 | 1976 | Voskhod | |||||
Vostok-L | Uni Soviet | RSC Energia | 4 | Retired | 1960 | 1960 | Vostok-L | |||||
Vostok-K | Uni Soviet | RSC Energia | 16 | Retired | 1960 | 1964[butuh rujukan] | Vostok-K | |||||
Vostok-2 | Uni Soviet | RSC Energia | 45 | Retired | 1962 | 1967[butuh rujukan] | Vostok-2 | |||||
Vostok-2M | Uni Soviet | RSC Energia | [butuh rujukan] | 93Retired | 1964 | 1991[butuh rujukan] | Vostok-2M | |||||
Soyuz/Vostok | Uni Soviet | RSC Energia | Retired | 1965 | 1966[butuh rujukan] | Soyuz/Vostok | ||||||
Zenit-2 | Uni Soviet Ukraina | Yuzhnoye | 13.740 | 37 | Retired | 1985 | 2004 | Zenit-2 | ||||
Zenit-2M (2SLB) | Ukraina | Yuzhnoye | 13.920 | 1 | Operational | 2007 | Zenit-2M (2SLB) | |||||
Zenit-3F | Ukraina | Yuzhnoye | 1 | Operational | 2011 | Zenit-3F | ||||||
Zenit-3SL | Ukraina | Yuzhmash RKK Energia | 6.000 to GTO | 100 | 30 | Operational | 1999 | Zenit-3SL | ||||
Zenit-3SLB | Ukraina | Yuzhmash RKK Energia | [butuh rujukan] | 3.750 to GTO[butuh rujukan] | 4Operational | 2008 | Zenit-3SLB |
Lihat pula Sunting
Catatan Sunting
- A full listing of the Ariane 5 launch history is in its main article.
- Suborbital test in 1969, first orbital launch attempt in 1970
- ^ 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.
- ^ 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) 2011-05-17 di 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.
- Suborbital test flight in 2004, first orbital launch in 2006
- A third rocket exploded before launch
- First orbital launch attempt in 2005
- ^ Operated by Land Launch
- Operated by Sea Launch
Referensi Sunting
- ^ . Khrunichev. Diarsipkan dari versi asli tanggal 2017-01-18. Diakses tanggal 2013-11-15.
- ^ European Space Directory 2006. Referenced in: Brian Harvey, The Rebirth of the Russian Space Program. p.296.
- ^ Семейство ракет-носителей «Ангара» 2017-01-18 di Wayback Machine., date unknown, Retrieved 2010-08-09.
- ^ "The Angara-7 rocket". Russianspaceweb.com. Diakses tanggal 2012-07-25.
- ^ Gunter, Krebs. "Ariane-1, -2, -3, -4". Gunter's Space Page. Diakses tanggal 2 August 2011.
- ^ (PDF). Arianespace. Diarsipkan dari versi asli (PDF) tanggal 2007-09-27. Diakses tanggal 2007-11-13.
- "Ariane 5 delivers a record performance with two payloads for new Arianespace customers". Arianespace. Diakses tanggal 2011-04-11.
- ^ "FAA Semi-Annual Launch Report: Second Half of 2009" (PDF). Federal Aviation Administration - Office of Commercial Space Transportation. hlm. end of document. Diakses tanggal August 18, 2011.
- "ESA - Launch vehicles - Ariane 5 ME". Esa.int. 2011-06-21. Diakses tanggal 2013-11-11.
- ^ "Ariane-5". Space.skyrocket.de. Diakses tanggal 2012-07-25.
- ^ "Final launch of Ariane 5 GS completes busy year / Launchers / Our Activities / ESA". Esa.int. 2009-12-19. Diakses tanggal 2013-11-04.
- . Isro.org. Diarsipkan dari versi asli tanggal 2014-10-29. Diakses tanggal 2013-11-04.
- "Athena-1". Astronautix.com. Diakses tanggal 2013-11-04.
- ^ . Diarsipkan dari versi asli tanggal 2010-03-28. Diakses tanggal 2013-11-15.
- "Athena-2". Astronautix.com. Diakses tanggal 2013-11-04.
- ^ Gunter, Krebs. "Atlas Centaur". Gunter's Space Page. Diakses tanggal 1 August 2011.
- ^ Gunter, Krebs. "Atlas-5". Gunter's Space Page. Diakses tanggal 1 August 2011.
- "CONTRACT RELEASE : C12-016: NASA Awards Launch Contract For Goes-R And Goes-S Missions". NASA. Diakses tanggal 2013-04-21.
- ^ Gunter, Krebs. "Delta". Gunter's Space Page. Diarsipkan dari versi asli tanggal 2011-08-02. Diakses tanggal 2 August 2011.
- Wade, Mark. "Delta 0300". Encyclopedia Astronautica. Diarsipkan dari versi asli tanggal 2011-08-02. Diakses tanggal 2 August 2011.
- Wade, Mark. "Delta 0900". Encyclopedia Astronautica. Diarsipkan dari versi asli tanggal 2011-08-02. Diakses tanggal 2 August 2011.
- ^ Wade, Mark. "Delta 2913". Encyclopedia Astronautica. Diarsipkan dari versi asli tanggal 2011-08-02. Diakses tanggal 2 August 2011.
- Wade, Mark. "Delta 4000". Encyclopedia Astronautica. Diarsipkan dari versi asli tanggal 2011-08-02. Diakses tanggal 2 August 2011.
- Wade, Mark. "Delta 5000". Encyclopedia Astronautica. Diarsipkan dari versi asli tanggal 2011-08-02. Diakses tanggal 2 August 2011.
- ^ (PDF). United Launch Alliance. Diarsipkan dari versi asli (PDF) tanggal 2007-09-28. Diakses tanggal 2007-11-14.
- "Breaking News | Lockheed Martin to select Delta 4 rocket for Orion test". Spaceflight Now. Diakses tanggal 2012-07-25.
- ^ Gunter, Krebs. "Delta-4". Gunter's Space Page. Diarsipkan dari versi asli tanggal 2011-08-02. Diakses tanggal 2 August 2011.
- ^ Ed Kyle. "Delta IV Data Sheet". Spacelaunchreport.com. Diakses tanggal 2013-11-04.
- "Delta Launch Report | New communications craft launched for U.S. military". Spaceflight Now. 2009-12-05. Diakses tanggal 2013-11-04.
- Gunter, Krebs. "Dnepr-1". Gunter's Space Page. Diarsipkan dari versi asli tanggal 2011-08-02. Diakses tanggal 2 August 2011.
- ^ . Energia. Diarsipkan dari versi asli tanggal 2016-03-03. Diakses tanggal 2013-11-15.
- Kesalahan pengutipan: Tag
<ref>
tidak sah; tidak ditemukan teks untuk ref bernamaEnergia3
- ^ . IHI Aerospace. Diarsipkan dari versi asli tanggal 2011-04-06. Diakses tanggal 2011-03-08.
- ^ "Satellite Launch Vehicles". Institute of Space and Astronautical Science (ISAS). Diakses tanggal 4 March 2011.
- "Breaking News | Japan's 'affordable' Epsilon rocket triumphs on first flight". Spaceflight Now. 2013-09-14. Diakses tanggal 2013-11-04.
- ^ . Diarsipkan dari versi asli tanggal 2013-04-05. Diakses tanggal 2010-10-29.
- ^ . SpaceX. Diarsipkan dari versi asli tanggal 2013-05-01. Diakses tanggal 2013-11-04.
- . Space Exploration Technologies. Diarsipkan dari versi asli tanggal 2007-10-13. Diakses tanggal 29 Oct 2010.
- "Falcon 9 Overview". SpaceX. 2011. Diarsipkan dari versi asli tanggal 2011-12-01. Diakses tanggal 2011-12-01.
- Klotz, Irene (2013-09-06). "Musk Says SpaceX Being "Extremely Paranoid" as It Readies for Falcon 9's California Debut". Space News. Diarsipkan dari versi asli tanggal 2013-09-22. Diakses tanggal 2013-11-04.
...the company’s five previous Falcon 9 boosters, all launched from Cape Canaveral Air Force Station here. Three of those rockets carried Dragon cargo capsules to the international space station for NASA. Two others were test flights.
- Clark, Stephen (2012-05-18). "Q&A with SpaceX founder and chief designer Elon Musk". Diakses tanggal 2013-11-04.
The next version of Falcon 9 will be used for everything. The last flight of version 1.0 will be Flight 5. All future missions after Flight 5 will be v1.1. We've got this mission, which is Flight 3. And we've two CRS [Commercial Resupply Services] missions, Flight 4 and Flight 5, which will fly Version 1.0. Then all future missions, CRS or otherwise, will fly Version 1.1.
- "FALCON 9 Launch Vehicle Performance". NASA. Diakses tanggal 2013-11-04.[pranala nonaktif permanen]
- "FALCON 9 Launch Vehicle Performance". NASA. Diakses tanggal 2013-11-04.[pranala nonaktif permanen]
- ^ "Upgraded Spacex Falcon 9.1.1 will launch 25% more than old Falcon 9 and bring price down to $4109 per kilogram to LEO". Nextbigfuture.com. 2013-03-22. Diakses tanggal 2013-11-04.
- ^ . SpaceX. 2013. Diarsipkan dari versi asli tanggal 2013-04-05. Diakses tanggal 2013-03-22.
- ^ "SpaceX Brochure" (PDF). Spacex.com. (PDF) dari versi asli tanggal 2010-01-07. Diakses tanggal 14 June 2011.
- . Isro.org. Diarsipkan dari versi asli tanggal 2013-11-11. Diakses tanggal 2013-11-04.
- . Isro.org. 2001-04-18. Diarsipkan dari versi asli tanggal 2013-11-11. Diakses tanggal 2013-11-04.
- . Isro.org. Diarsipkan dari versi asli tanggal 2013-11-11. Diakses tanggal 2013-11-04.
- . Isro.org. Diarsipkan dari versi asli tanggal 2013-08-22. Diakses tanggal 2013-11-04.
- . Isro.org. 2010-04-15. Diarsipkan dari versi asli tanggal 2010-04-16. Diakses tanggal 2013-11-04.
- "Welcome To ISRO :: Launch Vehicles :: GSLV". Isro.org. Diakses tanggal 2013-11-04.
- . Isro.gov.in. Diarsipkan dari versi asli tanggal 2013-08-11. Diakses tanggal 2013-11-04.
- . Indian Space Research Organisation. 2011. Diarsipkan dari versi asli tanggal 2012-11-25. Diakses tanggal 2012-08-12.
- ^ Gunter, Krebs. "H-2". Gunter's Space Page. Diakses tanggal 1 August 2011.
- ^ Gunter, Krebs. "H-2A". Gunter's Space Page. Diakses tanggal 1 August 2011.
- (PDF). Jaxa. Diarsipkan dari versi asli (PDF) tanggal 2009-07-30. Diakses tanggal 3 September 2008.
- ^ "Space Launch Report 2011 Launch Stats". Spacelaunchreport.com. Diakses tanggal 2013-11-04.
- ^ "NISSAN HERITAGE COLLECTION online【その他】プリンス自動車工業小史". Nissan Motors. Diakses tanggal 8 March 2011.
- "CZ-1". Astronautix.com. Diakses tanggal 2013-11-04.
- "[专题]中国大推力火箭技术已被日本大幅超越_网易新闻中心". War.news.163.com. Diakses tanggal 2013-11-04.
- ^ "长征三号甲运载火箭简述". Diakses tanggal 31 October 2011.
- ^ "CZ-4B (Chang Zheng-4B)". Space.skyrocket.de. Diakses tanggal 2013-11-04.
- ^ "ChangZheng 5 (Long March 5) Launch Vehicle". SinoDefence.com. 2009-02-20. Diakses tanggal 2009-03-06.
- Covault, Craig. "First Look: China's Big New Rockets « AmericaSpace". Americaspace.com. Diakses tanggal 2013-11-04.
- "Minotaur I Space Launch Vehicle—Fact Sheet" (PDF). Orbital Sciences Corporation. 2012. (PDF) dari versi asli tanggal 2006-10-18. Diakses tanggal 2012-02-28.
Spacecraft mass-to-orbit of up to 580 kg to LEO (28.5 deg, 185 km)
- "Minotaur Space Launch Vehicles". Orbital Sciences Corporation. 2012. Diakses tanggal 2012-08-28.
To date, Minotaur has conduced ten missions with a 100% success rate, delivering 33 satellites into orbit.
- ^ . Diarsipkan dari versi asli tanggal 2013-09-19. Diakses tanggal 2013-11-15.
- ^ "Molniya and Soyuz with upper stages". Space.skyrocket.de. Diakses tanggal 2013-11-04.
- Kesalahan pengutipan: Tag
<ref>
tidak sah; tidak ditemukan teks untuk ref bernamarefN1-1
- Kesalahan pengutipan: Tag
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tidak sah; tidak ditemukan teks untuk ref bernamarefN1-2
- Kesalahan pengutipan: Tag
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tidak sah; tidak ditemukan teks untuk ref bernamarefN1-3
- Kesalahan pengutipan: Tag
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tidak sah; tidak ditemukan teks untuk ref bernamarefN1-4
- ^ wikipedia, wiki, buku, buku, perpustakaan, artikel, baca, unduh, gratis, unduh gratis, mp3, video, mp4, 3gp, jpg, jpeg, gif, png, gambar, musik, lagu, film, buku, permainan, permainan.