From Wikipedia, the free encyclopedia
A Falcon Heavy launch vehicle from SpaceX
This comparison of orbital launch systems lists the attributes of all individual rocket configurations designed to reach orbit. A first list contains rockets that are operational or in development as of 2023; a second list includes all upcoming rockets and a third list includes all retired rockets For the simple list of all conventional launcher families, see: Comparison of orbital launchers families . For the list of predominantly solid-fueled orbital launch systems, see: Comparison of solid-fueled orbital launch systems .
Spacecraft propulsion [note 1] is any method used to accelerate spacecraft and artificial satellites . Orbital launch systems are rockets and other systems capable of placing payloads into or beyond Earth orbit . All launch vehicle propulsion systems employed to date have been chemical rockets falling into one of three main categories:
Solid-propellant rockets or solid-fuel rockets have a motor that uses solid propellants , typically a mix of powdered fuel and oxidizer held together by a polymer binder and molded into the shape of a hollow cylinder. The cylinder is ignited from the inside and burns radially outward, with the resulting expanding gases and aerosols escaping out via the nozzle.[note 2]
Liquid-propellant rockets have a motor that feeds liquid propellant(s) into a combustion chamber. Most liquid engines use a bipropellant , consisting of two liquid propellants (fuel and oxidizer) which are stored and handled separately before being mixed and burned inside the combustion chamber.
Hybrid-propellant rockets use a combination of solid and liquid propellant, typically involving a liquid oxidizer being pumped through a hollow cylinder of solid fuel.
All current spacecraft use conventional chemical rockets (solid-fuel or liquid bipropellant) for launch, though some[note 3] have used air-breathing engines on their first stage .[note 4]
Table code key:
Reusable Launch Vehicle
Expendable Launch Vehicle
Current rockets [ edit ]
Orbits legend:
LEO, low Earth orbit
SSO or SSPO, near-polar Sun-synchronous orbit
polar, polar orbit
MEO, medium Earth orbit
GTO, geostationary transfer orbit
GEO, geostationary orbit (direct injection)
HEO, high Earth orbit
HCO, heliocentric orbit
TLI, trans-lunar injection
TMI, trans-Mars injection
LMO Low Mars Orbit
Vehicle
Origin
Manufacturer
Height
Payload mass to ... (kg)
Orbital launches incl. failures[a]
Launch Site (s)
Date of flight
LEO
GTO
Other
First
Latest
Firefly Alpha
United States
Firefly Aerospace
29 m
1,000 [1]
630 to SSO
3
2021
2023
Angara A5
Russia
Khrunichev
55.4 m
24,500
5,400 with Briz-M [2] 7,500 with KVTK
3 [3]
2014
2021
Angara 1.2
Russia
Khrunichev
42.7 m
3,500 [2]
2,400 to SSO
2 [4]
2022
2022
Atlas V 501
United States
ULA
62.5 m
8,250 [5]
3,970
5,945 to SSO 1,500 to GEO
7 [5]
2010
2020
Atlas V 551
United States
ULA
58.3 m
18,500 [5]
8,700
13,550 to SSO 3,960 to GEO
13 [5]
2006
2021
Atlas V N22 [b]
United States
ULA
52.4 m
13,000
2
2019[7]
2022
Ceres-1 (3)[c]
China
Galactic Energy
20 m
400 [9]
300 to SSO[9]
7
2022
2023
Ceres-1S [d]
China
Galactic Energy
20 m
~ 400
1
Sea launch platform
2023
2023
Chollima-1
North Korea
NADA
26.2 m
> 300 [10]
2
2023
2023
Delta IV Heavy
United States
ULA
72 m
28,790 [11]
14,220
23,560 to polar 11,290 to TLI 8,000 to TMI
15 [12]
2004
2023
Electron
United States New Zealand
Rocket Lab
18 m
300 [13]
200 to SSO[13]
40 [14]
2017
2023
Epsilon
Japan
IHI [15]
24.4 m
1,500 [16]
590 to SSO
6 [17]
2013
2019
Falcon 9 Block 5
United States
SpaceX
70 m
17,400 -22,800
5,500 -8,300
200
2018
2023
Falcon Heavy [18]
United States
SpaceX
70 m
30,000 [19] –63,800
8,000 [20] –26,700
16,800 to TMI[21]
7 [22] [23]
Kennedy
2018
2023
GSLV Mk II
India
ISRO
49.1 m
5,000 [24]
2,700 [25] [e]
9 [26]
2010
2023
H-IIA 202
Japan
Mitsubishi
53 m
8,000 [27] : 67
4,000 [27] : 48
5,100 to SSO[f] [27] : 64–65
32[28]
2001
2023
H3-22S
Japan
Mitsubishi
57 m
[29]
3,500
1
2023
2023
Hyperbola-1 (2)[g]
China
i-Space
22.5 m
300 [31]
4
2021
2023
Jielong 1 [32]
China
CALT
19.5 m
N/A
200 to SSO
1 [32]
2019
2019
Jielong 3
China
CALT
31 m
N/A
1,500 (500 km SSO)
1 [33]
Sea launch platform
2022
2022
Kaituozhe-2
China
CASC
16.8 m
800 [34]
1 [34]
2017
2017
Kinetica 1
China
CAS Space
30 m
2,000 [35]
1,500 [36] TO 500 km SSO
2 [37]
2022
2023
Kuaizhou 1A
China
ExPace
19.8 m
200
250 to SSO
24
2013[h]
2023
Kuaizhou 11
China
ExPace
25.3 m
1,500 [39]
1,000 to SSO[40]
2
2020
2022
Long March 2C
China
CALT
42 m
3,850 [citation needed ]
1,250 with CTS2
2,000 to SSO with YZ-1 S[41]
71 [42]
1982
2023
Long March 2D
China
SAST
41.1 m
4,000
1,150 to SSO
80[42]
1992
2023
Long March 2F
China
CALT
62 m
8,600
20 [42]
1999
2023
Long March 3A
China
CALT
52.5 m
6,000 [43]
2,600
5,000 to SSO
27 [44]
1994
2018
Long March 3B/E
China
CALT
56.3 m
11,500 [43]
5,500
6,900 to SSO
79 [44]
2007
2023
Long March 3C
China
CALT
54.8 m
9,100 [43]
3,800
6,500 to SSO
18 [44]
2008
2021
Long March 4B
China
SAST
44.1 m
4,200 [45]
1,500
2,800 to SSO
48 [45]
1999
2023
Long March 4C
China
SAST
45.8 m
4,200 [46]
1,500
2,800 to SSO
53 [45]
2006
2023
Long March 5
China
CALT
56.9 m
25,000
14,000 [47]
15,000 to SSO[48] 9,400 to TLI[47] 6,000 to TMI[47]
5 [48]
2016
2020
Long March 5 B
China
CALT
56.9 m
25,000 [48]
4 [48]
2020[49]
2022
Long March 6
China
SAST
29 m
1,500 [50]
1,080 to SSO[51]
11 [52]
2015
2023
Long March 6A
China
SAST
50 m
Unknown
4,000 to SSO[53]
3 [52]
2022
2023
Long March 7
China
CALT
53.1 m
13,500 [54]
5,500 to SSO
7 [55]
2016[56]
2023
Long March 7A
China
CALT
60.13 m
N/A
5,500 to 7,000 [49]
5 [55]
2020
2023
Long March 8
China
CALT
50.34 m
8,400
2,800
5,000 to SSO
2 [57]
2020
2022
Long March 11
China
CALT
20.8 m
700 [58]
350 to SSO
16 [59]
2015
2023
LVM 3
India
ISRO
43.4 m
10,000 [60]
4,000
2,380 to TLI
7 [61]
2017[i]
2023
Minotaur-C (Taurus-3210) [63]
United States
Northrop Grumman
27.9 m
1,458 [64]
1,054 to SSO[j]
2
2004
2017
Minotaur I
United States
Northrop Grumman
19.2 m
580 [65]
12 [66]
2000
2021
Minotaur IV
United States
Northrop Grumman
23.9 m
1,735 [67]
5 [68] [k]
2010
2020
Minotaur V
United States
Northrop Grumman
24.6 m
N/A
670 [68]
465 to HCO
1 [68]
2013
2013
Nuri (KSLV-II)
South Korea
KARI
47.2 m
3,300 [69]
1,900 to SSO[70] [71] [69]
3 [71]
2021
2023
OS-M1
China
OneSpace
19 m
205 [72]
143 to SSO
1
2019[73] [l]
2019
Pegasus XL
United States
Northrop Grumman
16.9 m
544
35
1994
2021
Proton-M
Russia
Khrunichev
58.2 m
23,000 [75] [76]
6,150 (M) 6,920 (M+)
115 [77] [78] [79]
2001
2023
PSLV-CA
India
ISRO
44.4 m
2,100 [80]
1,100 to SSO
17 [80]
2007
2023
PSLV-DL
India
ISRO
44.4 m
N/A
750 to polar
1 [80]
2019
2021
PSLV-QL
India
ISRO
44.4 m
2 [80]
2019
2019
PSLV-XL
India
ISRO
44.4 m
3,800 [80]
1,300
1,750 to SSO550 to TMI [81]
25 [80]
2008
2023
Qased
Iran
Revolutionary Guard Corps (IRGC)
18.8 m
40 [82]
3
2020
2023
RS1
United States
ABL Space Systems
27 m
1,350 [83]
400
1,000 to SSO750 to MEO
1
2023[84]
2023
Shavit-2
Israel
IAI
22.1 m
400 in Retrograde
6
2007
2023
Simorgh
Iran
Iranian Space Agency
26 m
350 [85]
2 [85] [m]
2017
2021
Soyuz-2.1a
Russia
TsSKB-Progress
46.3 m
7,020 from Baikonur [86]
62 [87] [88] [89]
2006[n]
2023
Soyuz-2.1b
Russia
TsSKB-Progress
46.3 m
8,200 from Baikonur [86]
2,400 [90]
65 [88] [91]
2006
2023
Soyuz-2-1v
Russia
TsSKB-Progress
44 m
2,800 [92]
1,400 to SSO
10 [92]
2013
2023
Starship [93]
United States
SpaceX
122 m
150,000 [94] -250,000
1
2023
2023
SLS Block 1
United States
NASA / Boeing Northrop Grumman
98 m
95,000 [95]
27,000 + to TLI[96]
1
2022[97]
2022
SSLV
India
ISRO
34 m
500 [98]
300 to SSO
2 [99]
2022
2023
Tianlong-2
China
Space Pioneer
32.8 m
2,000 [100]
1,500 to SSO
1
2023
2023
Unha-3
North Korea
KCST
30 m
100 -110
4 [101]
2009[o]
2016
Vega
Europe
ESA / ASI
31 m
2,300 [102]
1,330 to SSO[103] 1,500 to polar[104]
15 [105]
2012
2020
Vega C
Europe
ESA / ASI
36.2 m
3,300 [106]
2,200 to SSO[106]
2 [107]
2022
2022
Zhuque-2
China
LandSpace
49.5 m
6,000 [108]
4,000 to SSO
2
2022[109]
2023
^ Suborbital flight tests and on-pad explosions are excluded, but launches failing en route to orbit are included.
^ for Starliner [6]
^ Despite not being officially aknowledged by the manifacturer, significant changes between different iterations of the rocket lead to the identification of different variants.[8]
^ Sea-launched version of the third unofficial iteration of the Ceres-1 launch vehicle.
^ GTO payload with enhanced engines, as of GSLV version 2A[26]
^ 5,100 kg to a 500-km Sun-synchronous orbit; 3,300 kg to 800 km[27] : 64–65
^ Despite not being officially aknowledged by the manifacturer, significant changes between different iterations of the rocket lead to the identification of different variants.[30]
^ A suborbital test flight was conducted in March 2012.[38]
^ A suborbital test flight was conducted in 2014 (designated LVM-3/CARE ) without the cryogenic upper stage (CUS).[62]
^ Reference altitude 400 km
^ Additionally, two suborbital missions were conducted in 2010 and 2011.[68]
^ A suborbital test flight was conducted in May 2018.[74]
^ A suborbital test flight succeeded in 2016; both orbital flights in 2017 and 2019 failed.[85]
^ Suborbital test flight in 2004, without Fregat upper stage.[87]
^ 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.[101]
Upcoming rockets [ edit ]
Upcoming North American launch vehicles
Vehicle
Origin
Manufacturer
Height
Payload mass to ... (kg)
Launch Site (s)
Date of first flight
LEO
GTO
Other
Antares 330
United States
Northrop Grumman /
Firefly Aerospace [a]
10,500
2025
Aurora
Canada
Reaction Dynamics
18 m
150
2024
Daytona
United States
Phantom Space
18.7 m
425
2023
Dauntless
United States
Vaya Space
35 m
1,000
CCSFS ,
Sea launch platform
2024
Laguna
United States
Phantom Space
20.5 m
630-1,200
TBA
MLV
United States
Firefly Aerospace
55.7 m
16,000
2025[110]
Neutron
United States New Zealand
Rocket Lab
42.8 m
13,000-15,000
2024[111]
New Glenn
United States
Blue Origin
98 m
45,000 [112]
13,000
2024
Mars Ascent Vehicle (MAV)
United States
NASA /
Northrop Grumman / Lockheed Martin
2.3 m
N/A
0.5 to LMO
2030
Ravn X
United States
aevum
24 m (drone)
9.8 m (rocket)
100
2024
Rocket 4
United States
Astra
18.9 m
600
2024
Shockwave
United States
iRocket
2,200
TBD
2027
SLS Block 1B [b]
United States
NASA / Boeing Northrop Grumman
111 m
105,000 [113]
37,000 to TLI[114]
2028
SLS Block 2 [c]
United States
NASA / Boeing Northrop Grumman
111 m
130,000 [115]
45,000 to HCO[114]
2033
Stoke Space launch vehicle
United States
Stoke Space
1,500
TBA
Terran R
United States
Relativity Space
82 m
23,500-33,500
5,500 [116]
2026[116]
Vector-R
United States
Vector Launch
12 m
60
26 to SSO
TBA
Vulcan Centaur VC0
United States
ULA
61.6 m
10,800
3,500
2,300 to TLI
2020s
Vulcan Centaur VC2
United States
ULA
61.6 m
19,000
8,400
2,600 to GEO 6,300 to TLI
2023[117]
Vulcan Centaur VC4
United States
ULA
61.6 m
24,600
11,700
4,900 to GEO 9,200 to TLI
2020s
Vulcan Centaur VC6
United States
ULA
61.6 m
27,200 [118]
14,400 [118]
6,500 to GEO 11,500 to TLI
2020s
Upcoming Chinese launch vehicles
Vehicle
Origin
Manufacturer
Height
Payload mass to ... (kg)
Launch
Site (s)
Date of first flight
LEO
GTO
Other
Darwin-1
China
Rocket Pi
27.2 m
470
TBD
2024
Gravity-1
China
Orienspace
31.4 m
6,500
4,200 to SSO
Sea launch platform
2023
Gravity-2
China
Orienspace
60 m
15,500
5,800
10,900 to SSO
TBA
2024
Hyperbola-2
China
i-Space
35.2 m
2,000 [31]
2024[36]
Kinetica 2
China
CAS Space
37 m
2,200
TBA
2024
Kinetica 3
China
CAS Space
53 m
6,100
TBA
2025
Long March 6C
China
CALT
43 m
4,500
TBA
2023
Long March 9
China
CALT
114 m
80,000 -150,000[119]
66,000 [120]
53,000 to TLI[119] 40,000 to TMI[121]
2033
Long March 10
China
CALT
89-93.2 m
70,000
27,000 to TLI
2027
Long March 10A
China
CALT
67 m
~ 14,000
>2027
Nebula-1
China
Deep Blue Aerospace
1,000
TBA
2024
OS-M2
China
OneSpace
390 [72]
292 to SSO
TBA
Pallas-1
China
Galactic Energy
42 m
5,000
3,000 to SSO
TBA
2024[122]
Space Chaser I
China
Nayuta space
67.3 m
10,000
TBD
TBA
Tianlong-3
China
Space Pioneer
71 m
17,000
2024
Upcoming European launch vehicles (without Russian launch vehicles)
Vehicle
Origin
Manufacturer
Height
Payload mass to ... (kg)
Launch Site (s)
Date of first flight
LEO
GTO
Other
Ariane 6 A62
Europe
ArianeGroup
63 m
10,350 [123] : 45
5,000 [123] : 33
6,450 to SSO 3,000 to HEO 3,000 to TLI [123] : 40–49
2024[124]
Ariane 6 A64
Europe
ArianeGroup
63 m
21,650 [123] : 46
11,500 + [123] : 33
14,900 to SSO 5,000 to GEO 8,400 to HEO 8,500 to TLI [123] : 40–49
2024[124]
Cyclone-4M
Ukraine
Yuzhnoye Yuzhmash
38.7 m
5,000 [125]
1,000 [126]
3,350 to SSO[125]
2025[127]
Hera II
United Kingdom
Astraius , Northrop Grumman ,
Exquadrum [128]
~26 m
800
2024
MaiaSpace launch vahicle
France
MaiaSpace
23.5 m
500
2025
Miura 5
Spain
PLD Space
29.4 m
840
450 to SSO
2024[129]
Prime
United Kingdom
Orbex
19 m
220 [130]
150 to SSO[d] [131]
2023[132]
RFA One
Germany
RFA
30 m
1,600 [133]
450 [133]
2024[134]
ŞİMŞEK-1
Turkey
Roketsan
TBA
400
2027
Skyrora XL
United Kingdom
Skyrora
22.7 m
335 [135]
315 to SSO[135]
2024
SL1
Germany
HyImpulse
27 m
500
2025
Spectrum
Germany
Isar Aerospace
28 m
1,000 [136]
700 to SSO[136]
2023[137]
Vega E
Europe
ESA / ASI
36.2 m
3,000 [138]
2026
Zephyr
France
Latitude
17 m
72
2026
Upcoming Russian launch vehicles
Vehicle
Origin
Manufacturer
Height
Payload mass to ... (kg)
Launch
Site (s)
Date of first flight
LEO
GTO
Other
Amur (Soyuz-7)
Russia
JSC SRC Progress
55 m
10,500 -13,600 [139]
2,600
4,700 to SSO
2028-2030
Angara A5M
Russia
Khrunichev
55.4 m
26,800
4,100 -5,200
2025
Angara A5P
Russia
Khrunichev
TBA
18,800
N/A
2025
Angara A5V
Russia
Khrunichev
70 m
37,500
8,000
TBD
2027
Cosmos
Russia
SR space
18.5 m
100
TBD
Rokot-M
Russia
Khrunichev
TBA
1,950
2024
Irtysh (Soyuz-5)
Russia
TsSKB-Progress RSC Energia
61.87 m
18,000 [140]
2,500 to GEO
2025[141]
Stalker
Russia
SR space
32.8 m
950
2024
Volga (Soyuz-6)
Russia
TsSKB-Progress
TBA
9,300
2,300
5,500
2025
Yenisei [142]
Russia
TsSKB-Progress RSC Energia
~80 m
88,000 – 115,000[143]
27,000 to TLI[144] [145] [146]
2030s
Upcoming Indian launch vehicles
Upcoming East and South Asian launch vehicles
Upcoming South American launch vehicles
Upcoming Australian launch vehicles
Upcoming Iranian launch vehicles
^ provides the first stage, including engines
^ with EUS
^ with EUS and advanced boosters
^ a b Reference altitude 500 km
Retired rockets [ edit ]
Vehicle
Origin
Manufacturer
Height
Mass to ... (kg)
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 [156]
1,500 to SSO
5 [156]
2013
2014
Antares 230 / 230+
United States
Northrop Grumman
42.5 m
8,200 [156]
3,000 to SSO[a]
13
2016
2023
Ariane 1
Europe
Aérospatiale
49.1 m
1,830 [157]
11 [157]
1979
1986
Ariane 2
Europe
Aérospatiale
49.1 m
2,270 [157]
6 [157]
1986
1989
Ariane 3
Europe
Aérospatiale
49.1 m
2,650 [157]
11 [157]
1984
1989
Ariane 4 40
Europe
Aérospatiale
58.7 m
4,600 [157]
2,105
2,740 to SSO
7 [157]
1990
1999
Ariane 4 42L
Europe
Aérospatiale
58.7 m
7,000 [157]
3,480
4,500 to SSO
13 [157]
1993
2002
Ariane 4 42P
Europe
Aérospatiale
58.7 m
6,000 [157]
2,930
3,400 to SSO
15 [157]
1990
2002
Ariane 4 44L
Europe
Aérospatiale
58.7 m
7,000 [157]
4,720
6,000 to SSO
40 [157]
1989
2003
Ariane 4 44LP
Europe
Aérospatiale
58.7 m
7,000 [157]
4,220
5,000 to SSO
26 [157]
1988
2001
Ariane 4 44P
Europe
Aérospatiale
58.7 m
6,500 [157]
3,465
4,100 to SSO
15 [157]
1991
2001
Ariane 5 G
Europe
EADS Astrium
47.5 m
18,000 [158]
6,900 [158]
16 [158]
1996
2003
Ariane 5 G+
Europe
EADS Astrium
48 m
7,100 [158]
3 [158]
2004
2004
Ariane 5 GS
Europe
EADS Astrium
48 m
16,000 [159]
6,600 [158]
6 [158]
2005
2009[160]
Ariane 5 ES
Europe
EADS Astrium
50.7 m
21,000 [161]
8,000 [158]
8 [158]
2008
2018
Ariane 5 ECA
Europe
EADS Astrium
52.6 m
21,000 [161]
11,210 [162]
84
2002
2023
ASLV
India
ISRO [163]
23.5 m
150 [164]
4 [164]
1987
1994
Athena I
United States
Lockheed Martin
18.9 m
795 [165]
515
4 [166]
1995
2001
Athena II
United States
Lockheed Martin
28.2 m
1,800 [167]
3 [168]
1998
1999[169]
Atlas-Able
United States
General Dynamics
28 m
~175 to TLI
3
1959
1960
Atlas-Agena
United States
Convair /General Dynamics
36 m
1,000
390 to TLI
109
1960
1978
Atlas-Centaur
United States
Lockheed
36.2-38.8 m
1,134 [170]
2,222 [171]
148
1962
1983
Atlas B
United States
Lockheed Martin
24.9 m
~4,000
10
1958
1959
Atlas-D OV1
United States
Convair /General Dynamics
25.9 m
1,400
7
1965
1967
Atlas E/F- Agena
United States
Convair /General Dynamics /Lockheed
34 m
1,000
390 to TLI
1
1978
1978
Atlas E/F- Altair-3A
United States
Convair /General Dynamics
27.3 m
210
1
1990
1990
Atlas E/F- Burner-2
United States
Convair /General Dynamics
28.9 m
950
1
1972
1972
Atlas E/F-MSD
United States
Convair /General Dynamics
27.3 m
800
4
1976
1980
Atlas E/F-OIS
United States
Convair /General Dynamics
28.7 m
870
2
1979
1985
Atlas E/F- OV1
United States
Convair /General Dynamics
26.5 m
363
4
1968
1971
Atlas E/F-PTS
United States
Convair /General Dynamics
26.5 m
295
1
1974
1974
Atlas E/F-SGS-1
United States
Convair /General Dynamics
29 m
450
8
1977
1981
Atlas E/F-SGS-2
United States
Convair /General Dynamics
29 m
770
4
1983
1985
Atlas E/F- Star-17A
United States
Convair /General Dynamics
27.4 m
N/A
800 to MPEO
1
1975
1975
Atlas E/F- Star-37S
United States
Convair /General Dynamics
29 m
N/A
1,100 to SSO
19
1978
1995
Atlas-F Agena-D
United States
Convair /General Dynamics
34 m
N/A
2,300 to Polar
1
1978
1978
Atlas G
United States
Lockheed
43.9 m
5,900 [172]
2,222
1,179 to HCO[172]
7 [172]
1984
1989
Atlas H MSD
United States
Lockheed
27 m
3,630 [173]
5
1983
1987
Atlas LV-3B
United States
Convair
28.7 m
1,360
9
1960
1963
Atlas SLV-3
United States
Convair
33.3 m
63
1966
1983
Atlas SLV-3 Burner-2
United States
Convair
30.3 m
~1,000
1
1968
1968
Atlas I
United States
Lockheed Martin
43.9 m
5,900 [172]
2,340 [172]
11 [172]
CCSFS
1990
1997
Atlas II
United States
Lockheed Martin
47.5 m
6,780 [172]
2,810
2,000 to HCO[172]
10 [172]
VAFB, CCSFS
1991
1998
Atlas II A
United States
Lockheed Martin
47.5 m
7,316 [172]
3,180
2,160 to HCO[172]
23 [172]
VAFB, CCSFS
1992
2002
Atlas II AS
United States
Lockheed Martin
49 m
8,618 [172]
3,833
2,680 to HCO[172]
30 [172]
VAFB, CCSFS
1993
2004
Atlas III A
United States
Lockheed Martin
52.5 m
8,686 [172]
4,060
2,970 to HCO[172]
2 [172]
CCSFS
2000
2004
Atlas III B/DEC
United States
Lockheed Martin
53.7 m
10,759 [172]
4,609 [172]
1 [172]
CCSFS
2002
2002
Atlas III B/SEC
United States
Lockheed Martin
54.7 m
10,218 [174]
4,193 [172]
3 [172]
CCSFS
2003
2005
Atlas V 401
United States
ULA
57.3 m
9,050 [5]
4,950
6,670 to SSO
41 [5]
VAFB, CCSFS
2002
2022
Atlas V 411
United States
ULA
58.2 m
9,050 [5]
6,075
8,495 to SSO
6 [5]
VAFB, CCSFS
2006
2020
Atlas V 421
United States
ULA
59.1 m
9,050 [5]
7,000
9,050 to SSO
9 [5]
VAFB, CCSFS
2007
2022
Atlas V 431
United States
ULA
59.1 m
9,050 [5]
7,800
9,050 to SSO
3 [5]
VAFB, CCSFS
2005
2016
Atlas V 511
United States
ULA
62.5 m
11,000 [5]
5,250
7,820 to SSO 1,750 to GEO
1 [175]
VAFB, CCSFS
2022
2022
Atlas V 521
United States
ULA
59.7 m
13,300 [5]
6,485
9,585 to SSO 2,760 to GEO
2 [5]
VAFB, CCSFS
2003
2004
Atlas V 531
United States
ULA
59.7 m
15,300 [5]
7,425
11,160 to SSO 3,250 to GEO
5 [5]
VAFB, CCSFS
2010
2022
Atlas V 541
United States
ULA
59.7 m
17,100 [5]
8,240
12,435 to SSO 3,730 to GEO
9 [5]
VAFB, CCSFS
2011
2022
Black Arrow
United Kingdom
RAE
13 m
73 [176]
2 (+2)
WRC
1969[b]
1971
Blue Scout II
United States
Vought
24 m
30
3
CCSFS
1961
1961
Ceres-1 (1)[c]
China
Galactic Energy
18.5 m
350
1
JSLC
2020
2020
Ceres-1 (2)[c]
China
Galactic Energy
19.5 m
400
1
JSLC
2021
2021
Commercial Titan III
United States
Martin Marietta
47.3 m
13,100 [177]
4
CCSFS
1990
1992
Conestoga 1620
United States
Space Services
15.2 m
1179
1
MARS
1995
1995
Delta 0300
United States
McDonnell Douglas
34 m
340 [178]
747 to SSO[179]
3 [180]
VAFB
1972
1973[181]
Delta 0900
United States
McDonnell Douglas
34 m
1,300 [182]
818 to SSO[180]
2 [180]
VAFB
1972
1972
Delta 1410
United States
McDonnell Douglas
35.2 m
340 [183]
1 [180]
VAFB
1975
1975
Delta 1604
United States
McDonnell Douglas
35.2 m
390 [184]
2 [180]
CCSFS
1972
1973
Delta 1900
United States
McDonnell Douglas
35.2 m
1,800 [180]
1 [180]
VAFB
1973
1973
Delta 1910
United States
McDonnell Douglas
35.2 m
1,066 [185]
1 [180]
CCSFS
1975
1975
Delta 1913
United States
McDonnell Douglas
35.2 m
328 [186]
1 [180]
CCSFS
1973
1973
Delta 1914
United States
McDonnell Douglas
35.2 m
680 [187]
2 [180]
CCSFS
1972
1973
Delta 2310
United States
McDonnell Douglas
35.2 m
336 [188]
3 [180]
VAFB, CCSFS
1974
1981
Delta 2313
United States
McDonnell Douglas
35.2 m
243 to GEO[189]
3 [180]
VAFB, CCSFS
1974
1977
Delta 2910
United States
McDonnell Douglas
35.2 m
1,887 [180]
6 [180]
VAFB, CCSFS
1975
1978
Delta 2913
United States
McDonnell Douglas
35.2 m
2,000 [190]
700 [190]
6 [180]
VAFB, CCSFS
1975
1976
Delta 2914
United States
McDonnell Douglas
35.2 m
724 [180]
30 [180]
VAFB, CCSFS
1974
1979
Delta 3910
United States
McDonnell Douglas
35.2 m
2,494 [180]
1,154 with PAM-D
10 [180]
VAFB, CCSFS
1980
1988
Delta 3913
United States
McDonnell Douglas
35.2 m
816 [191]
1 [180]
VAFB, CCSFS
1981
1981
Delta 3914
United States
McDonnell Douglas
35.2 m
954 [180]
13 [180]
VAFB, CCSFS
1975
1987
Delta 3920
United States
McDonnell Douglas
35.2 m
3,452 [180]
1,284 with PAM-D
10 [180]
VAFB, CCSFS
1982
1989
Delta 3924
United States
McDonnell Douglas
35.2 m
1,104 [180]
4 [180]
VAFB, CCSFS
1982
1984
Delta 4925
United States
McDonnell Douglas
35.2 m
3,400 [192]
1,312 [180]
2 [180]
VAFB, CCSFS
1989
1990
Delta 5920
United States
McDonnell Douglas
35.2 m
3,848 [193]
1 [180]
VAFB
1989
1989
Delta II 6920
United States
McDonnell Douglas
38.8 m
3,983 [180]
3 [180]
VAFB, CCSFS
1990
1992
Delta II 6925
United States
McDonnell Douglas
39.4 m
1,447
1,447 [180]
14 [180]
VAFB, CCSFS
1989
1992
Delta II 7320
United States
Boeing IDS / ULA
38.9 m
2,865 [180]
1,651 to SSO
12 [180]
VAFB, CCSFS
1999
2015
Delta II 7326
United States
Boeing IDS
38.4 m
934 [180]
636 to TLI 629 to HCO
3 [180]
VAFB, CCSFS
1998
2001
Delta II 7420
United States
ULA
39 m
3,185 [180]
1,966 to SSO
14 [180]
VAFB, CCSFS
1998
2018
Delta II 7425
United States
Boeing IDS
39 m
1,100 [180]
804 to HCO
4 [180]
VAFB, CCSFS
1998
2002
Delta II 7426
United States
Boeing IDS
39 m
1,058 [180]
734 to TLI 711 to HCO
1 [180]
VAFB, CCSFS
1999
1999
Delta II 7920
United States
Boeing IDS / ULA
39.4 m
5,030 [180]
3,123 to SSO
29 [180]
VAFB, CCSFS
1998
2017
Delta II 7925
United States
Boeing IDS / ULA
39.4 m
1,819 [180]
1,177 to TLI 1,265 to HCO
69 [180]
VAFB, CCSFS
1990
2009
Delta II-H 7920H
United States
Boeing IDS / ULA
39 m
6,097 [180]
3 [180]
VAFB, CCSFS
2003
2011
Delta II-H 7925H
United States
Boeing IDS / ULA
39.8 m
2,171
1,508 to HCO[180]
3 [180]
VAFB, CCSFS
2003
2007
Delta III 8930
United States
Boeing IDS
39 m
8,292 [180]
3,810
3 [180]
CCSFS
1998
2000
Delta IV M
United States
Boeing IDS
61.3 m
9,440 [11]
4,440
7,690 to polar
3 [12]
VAFB, CCSFS
2003
2006
Delta IV M+(4,2)
United States
ULA
61.3 m
13,140 [11]
6,390
10,250 to polar
14 [12]
VAFB, CCSFS
2002
2019
Delta IV M+(5,2)
United States
ULA
65.5 m
11,470 [11]
5,490
9,600 to polar
3 [12]
VAFB, CCSFS
2012
2018
Delta IV M+(5,4)
United States
ULA
65.5 m
14,140 [11]
7,300
11,600 to polar
8 [12]
VAFB, CCSFS
2009
2019
Diamant A
France
SEREB
18.9 m
80
4
CIEES
1965
1967
Diamant B
France
SEREB
23.5 m
115
5
CSG
1970
1973
Diamant BP4
France
SEREB
21.6 m
153
3
CSG
1975
1975
Dnepr
Ukraine
Yuzhmash
34.3 m
3,700 [194]
22 [194]
Baikonur , Yasny
1999
2015[195]
Energia [d]
Soviet Union
NPO Energia
58.8 m
105,000
20,000 to GEO [196] 32,000 to TLI[196]
1 (failed to orbit)[197]
Baikonur
1987
1987
Energia -Buran
Soviet Union
NPO Energia (Launcher)NPO Molniya (Orbiter )
58.8 m
30,000 [196] [e]
1
Baikonur
1988
1988
Europa I
Europe
ELDO
31.7 m
1,440
200
3
WRC
1968
1970
Europa II
Europe
ELDO
31.7 m
360
1
CSG
1971
1971
Falcon 1
United States
SpaceX
21 m
470 [198]
5 [198]
Omelek
2006
2009
Falcon 9 v1.0
United States
SpaceX
47.8 m
9,000
3,400
5
VAFB, CCSFS
2010
2013
Falcon 9 v1.1
United States
SpaceX
68.4 m
13,150 [199] [f]
4,850 [199]
15 [200]
VAFB, CCSFS
2013
2016
Falcon 9 Full Thrust
United States
SpaceX
70 m
17,400-22,800 [20]
5,500-8,300 [20]
9,600 to polar[201]
223
VAFB, CCSFS , KSC
2015
2022
Feng Bao 1
China
Shanghai Bureau No.2
33 m
2,500 [202]
8 (+3)[203]
JSLC
1972
1981
GSLV Mk.I(a)
India
ISRO
49.1 m
5,000 [24]
1,540 [204]
1 [204]
SDSC
2001
2001
GSLV Mk.I(b)
India
ISRO
49.1 m
5,000 [24]
2,150 [204]
4 [204]
SDSC
2003
2007
GSLV Mk.I(c)
India
ISRO
49.1 m
5,000 [24]
1 [204]
SDSC
2010
2010
H-I
Japan United States
Mitsubishi
42 m
1,400 [205]
9
TNSC
1986
1992
H-II / IIS
Japan
Mitsubishi
49 m
10,060 [206]
4,000 [207]
7 [207]
TNSC
1994
1999
H-IIA 204
Japan
Mitsubishi
53 m
15,000
5,950 [27] : 48
5 [28]
TNSC
2006
2021
H-IIA 2022
Japan
Mitsubishi
53 m
4,500 [28]
3 [28]
TNSC
2005
2007
H-IIA 2024
Japan
Mitsubishi
57 m
11,000 [208]
5,000 [28]
7 [28]
TNSC
2002
2008
H-IIB
Japan
Mitsubishi
56.6 m
16,500 (ISS )[209]
8,000
8 [210]
TNSC
2009
2020
Hyperbola-1 (1)[g]
China
i-Space
20.9 m
260
1
JSLC
2019
2019
Juno I
United States
Chrysler
21.2 m
11
1
CCSFS
1958
1959
Juno II
United States
Chrysler
24 m
41
6 to TLI
10
CCSFS
1958
1961
Kaituozhe-1
China
CALT
13.6 m
40
2
JSLC
2002
2003
Kosmos
Soviet Union
NPO Polyot
29.6 m
350
38
Kapustin Yar
1961
1967
Kosmos-1
Soviet Union
NPO Polyot
26.3 m
1,400
8
Baikonur
1964
1965
Kosmos-2
Soviet Union
NPO Polyot
31 m
300
127
Kapustin Yar , Plesetsk
1965
1977
Kosmos-3
Soviet Union
NPO Polyot
32.4 m
1,400
6
Baikonur
1966
1968
Kosmos-3M
Soviet Union Russia
NPO Polyot
32.4 m
1,500 [211]
445
Kapustin Yar , Plesetsk
1967
2010
Kosmos-3MRB
Soviet Union
NPO Polyot
32.4 m
1,500
10
Kapustin Yar
1980
1988
Lambda 4S
Japan
Nissan Motors [212]
16.5 m
26 [213]
5
KSC
1966
1970
LauncherOne
United States
Virgin Orbit
21.3 m
500
300 to SSO
6
Mojave ,
Newquay
2020
2023
Long March 1
China
CALT
29.9 m
300 [214]
2 [215]
JSLC
1970
1971
Long March 1D
China
CALT
28.2 m
740 [216]
0 (+3)[215]
TSLC
1995[h]
2002
Long March 2A
China
CALT
32 m
2,000 [217]
4 [42]
JSLC
1974
1978
Long March 2E
China
CALT
49.7 m
9,200 [42]
7 [42]
XSLC
1990
1995
Long March 3
China
CALT
43.3 m
5,000 [44]
13 [44]
XSLC
1984
2000
Long March 3B
China
CALT
54.8 m
11,200 [43]
5,100
5,700 to SSO
12 [44]
XSLC
1996
2012
Long March 4A
China
CALT
41.9 m
4,000
2 [45]
TSLC
1988
1990
M-V
Japan
Nissan Motors [212] (1997–2000)IHI Aerospace [15] (2000–2006)
30.8 m
1,850 [213]
7
KSC
1997
2006
Molniya
Soviet Union
RSC Energia
43.4 m
1,800 [218]
40 [219]
Baikonur, Plesetsk
1960
1967
Molniya-M
Soviet Union Russia
RSC Energia
43.4 m
2,400 [220]
280 [221]
Baikonur, Plesetsk
1965
2010
Mu-4S
Japan
Nissan Motors [212]
23.6 m
180 [213]
4
KSC
1971
1972
Mu-3C
Japan
Nissan Motors [212]
20.2 m
195 [213]
4
KSC
1974
1979
Mu-3H
Japan
Nissan Motors [212]
23.8 m
300 [213]
3
KSC
1977
1978
Mu-3S
Japan
Nissan Motors [212]
23.8 m
300 [213]
4
KSC
1980
1984
Mu-3SII
Japan
Nissan Motors [212]
27.8 m
770 [213]
8
KSC
1985
1995
N1
Soviet Union
NPO Energia
105.3 m
95,000 [222] [223] [224] [i]
4 [225] (never reached orbit)
Baikonur
1969
1972
N-I
Japan United States
Mitsubishi
34 m
1,200 [226]
7
TNSC
1975
1982
N-II
Japan United States
Mitsubishi
35 m
2,000 [227]
8
TNSC
1981
1987
Naro-1
South Korea Russia
KARI /Khrunichev
33 m
100 [228]
3
Naro
2009
2013
Paektusan-1
North Korea
KCST
25.8 m
20
1
Tonghae
1998
1998
Pegasus
United States
Northrop Grumman
15.4 m
455
6
Edwards, CCSFS
1990
1994
Pegasus H
United States
Northrop Grumman
15.4 m
544
4
VAFB, CCSFS , Kwajalein Atoll
1995
2000
Pilot II
United States
United States Navy
4.4 m
N/A
1.05 to MEO
10
Point Mugu
1958
1958
Polyot
Soviet Union
RSC Energia
30 m
1,400
2
Baikonur
1963
1964
Proton (UR-500)
Soviet Union
Khrunichev
39.8 m
12,200
4
Baikonur
1965
1966
Proton-K
Soviet Union Russia
Khrunichev
50 m
19,760 [229]
4,930 [230]
311 [231]
Baikonur
1965
2012
PSLV-G
India
ISRO
44 m
3,200 [80]
1,050
1,600 to SSO
12 [80]
SDSC
1993
2016[232]
Rocket 3.0
United States
Astra
11.6 m
100
1
KLC
2020
2020
Rocket 3.1
United States
Astra
11.6 m
100
1
KLC
2020
2020
Rocket 3.2
United States
Astra
11.6 m
100
1
KLC
2020
2020
Rocket 3.3
United States
Astra
13.1 m
100 [233]
150 to SSO
5
CCSFS,
KLC
2021
2022
Rokot-K
Russia
Khrunichev
25.5 m
4
Baikonur, Plesetsk
1990
1999
Rokot-KM
Russia
Khrunichev
29.1 m
1,950 [234]
1,200 to SSO
31
Plesetsk
2000
2019
Safir-1
Iran
Iranian Space Agency
22.6 m
27
2
Semnan
2008
2009
Safir-1A
Iran
Iranian Space Agency
22.6 m
15
1
Semnan
2011
2011
Safir-1B
Iran
Iranian Space Agency
22.6 m
50
1
Semnan
2012
2012
Safir-1B+
Iran
Iranian Space Agency
22.6 m
52
5
Semnan
2012
2019
Saturn I
United States
Chrysler (S-I)Douglas (S-IV )
50-57.4 m
9,000 [235]
10 [236]
CCSFS
1961
1965[236]
Saturn IB
United States
Chrysler (S-IB )Douglas (S-IVB )
56.1-68.1 m
18,600 [237]
9 [238]
CCSFS , KSC
1966
1975
Saturn V
United States
Boeing (S-IC )North American (S-II )Douglas (S-IVB )
110.6 m
140,000 [239] [240]
47,000 to TLI[241]
13 [242] [243] [j]
KSC
1967
1973
Scout X-1
United States
Vought
21.8 m
59
4
MARS
1960
1961
Scout X-2
United States
Vought
21.8 m
76
1
VAFB , MARS
1962
1962
Scout X-2M
United States
Vought
21.8 m
76
3
VAFB
1962
1963
Scout X-2B
United States
Vought
21.8 m
76
1
VAFB
1963
1963
Scout X-3
United States
Vought
21.8 m
87
5
VAFB , MARS
1962
1964
Scout X-3M
United States
Vought
21.8 m
87
1
VAFB
1963
1963
Scout X-4
United States
Vought
22.8 m
103
11
VAFB , MARS
1963
1965
Scout A
United States
NASA
22.8 m
110
11
VAFB
1965
1970
Scout A-1
United States
NASA
22.8 m
122
1
VAFB
1973
1973
Scout B
United States
NASA
22.8 m
110
20
BSC ,
VAFB , MARS
1965
1971
Scout B-1
United States
NASA
22.8 m
143
5
BSC ,
VAFB , MARS
1971
1976
Scout D-1
United States
NASA
22.9 m
182
14
BSC ,
VAFB , MARS
1972
1979
Scout E-1
United States
NASA
22.8 m
193
1
VAFB
1974
1974
Scout F-1
United States
NASA
22.9 m
192
2
BSC ,
VAFB
1975
1975
Scout G-1
United States
NASA
22.9 m
208
18
BSC ,
VAFB , MARS
1979
1994
Shavit
Israel
IAI
17.7 m
160
2
Palmachim
1988
1990
Shavit-1
Israel
IAI
19.7 m
225
4
Palmachim
1995
2004
Shtil-1
Russia
Makeyev
14.8 m
280–420[244]
2 [245]
Barents Sea
1998
2006
SLV
India
ISRO
22 m
40 [246]
4 [246]
SDSC
1979
1983[246]
Soyuz
Soviet Union
RSC Energia
45.6 m
6,450
31 [247]
Baikonur
1966
1976
Soyuz-FG
Russia
TsSKB-Progress
49.5 m
6,900 [248]
70 [88] [249]
Baikonur
2001
2019
Soyuz-L
Soviet Union
RSC Energia
50 m
5,500
3 [250]
Baikonur
1970
1971
Soyuz-M
Soviet Union
RSC Energia
50 m
6,600
8 [251]
Plesetsk
1971
1976
Soyuz ST-A
Russia Europe
TsSKB-Progress Arianespace
46.3 m
7,800 from Kourou [252]
2,810 with Fregat [253]
9 [88]
CSG
2011
2021
Soyuz ST-B
Russia Europe
TsSKB-Progress Arianespace
46.3 m
9,000 from Kourou [254]
3,250 with Fregat [253]
4,400 to SSO[255]
18 [88]
CSG
2011
2022
Soyuz-U
Soviet Union Russia
TsSKB-Progress
51.1 m
6,650 from Baikonour [256] 6,150 from Plesetsk [256]
786 [88] [89] [257]
Baikonur, Plesetsk
1973
2017
Soyuz-U2
Soviet Union Russia
TsSKB-Progress
34.5 m
7,050
72 [258]
Baikonur
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 [259]
135 [261]
KSC
1981
2011
SPARK
United States
UH Aerojet Rocketdyne Sandia
17 m
300
1
Barking Sands
2015
2015
Sparta
United States
ABMA /Chrysler
21.8 m
45
10
WRC
1966
1967
Sputnik 8K71PS
Soviet Union
RSC Energia
30 m
500 [262]
2
Baikonur
1957
1957
Sputnik 8A91
Soviet Union
RSC Energia
31.1 m
1,327
2
Baikonur
1958
1958
SS-520
Japan
IHI Aerospace
9.5 m
4 [263]
2 [264]
KSC
2017[265] [k]
2018
Start-1
Russia
MITT
22.7 m
532
250 to SSO
5 [266]
Svobodny , Plesetsk
1993
2006
Start-1.2
Russia
MITT
22.7 m
250-300 to SSO
1
Svobodny
1997
1997
Start
Russia
MITT
28.9 m
300 to SSO
1
Plesetsk
1995
1995
Strela
Russia
Khrunichev
24-
27.4 m
1,400 [267]
3 [268]
Baikonur
2003
2014
Taurus-1110
United States
Orbital
Sciences , Orbital ATK
28.2 m
1180
370
750 to SSO
3
VAFB
1994
2000
Taurus-2110
United States
Orbital
Sciences , Orbital ATK
29.1 m
1250
375
900 to SSO
2
VAFB
1999
2001
Taurus-2210
United States
Orbital
Sciences , Orbital ATK
30.9 m
1050
700 to SSO
1
VAFB
1998
1998
Taurus-3110
United States
Orbital
Sciences , Orbital ATK
30.1 m
1450
445
1,050 to SSO
2
VAFB
2009
2011
Terran 1
United States
Relativity Space
35.2 m
1,250 [269]
900 to SSO
1
CCSFS
2023
2023
Titan II GLV
United States
Martin Marietta
33 m
3,600 [270]
11 (+1)
CCSFS
1964
1966
Titan II(23)G
United States
Martin Marietta
31.4 m
3,600 [271]
13
VAFB
1988
2003
Titan IIIA
United States
Martin Marietta
38.5 m
3,500
4
CCSFS
1964
1965
Titan IIIB
United States
Martin Marietta
42 m
3,300
22
VAFB
1966
1969
Titan III(23)B
United States
Martin Marietta
42 m
3,350
9
VAFB
1969
1971
Titan III(33)B
United States
Martin Marietta
42 m
N/A
4,500
3
VAFB
1971
1973
Titan III(24)B
United States
Martin Marietta
44 m
4,500
23
VAFB
1971
1984
Titan III(34)B
United States
Martin Marietta
45.3 m
N/A
11
VAFB
1975
1987
Titan IIIC
United States
Martin Marietta
41 m
11,500
3,000
14
CCSFS
1965
1970
Titan III(23)C
United States
Martin Marietta
42.5 m
13,100 [272]
3,000
22
CCSFS
1970
1982
Titan IIID
United States
Martin Marietta
36 m
12,300 [273]
22
VAFB
1971
1982
Titan IIIE
United States
Martin Marietta
48.8 m
15,400 [274]
7
CCSFS
1974
1977
Titan 34D
United States
Martin Marietta
44.5 m
14,350
3,600
15
VAFB, CCSFS
1982
1989
Titan IV A
United States
Martin Marietta
51.36 m (standard)
17,110 [275]
4,944 with IUS
14,090 to SSO[276]
4,536 to GSO with Centaur
3,550 to escape with IUS
22 [277]
VAFB, CCSFS
1989
1998
Titan IV B
United States
Lockheed Martin
51.36 m (standard)
21,682 [278]
5,761 [278] (9,000 with upper stage)
17 [277]
VAFB, CCSFS
1997
2005
Thor-Able I
United States
Douglas /Aerojet
26.9 m
250
3
CCSFS
1958
1958
Thor-Able II
United States
Douglas /Aerojet
27.3 m
270
4
CCSFS
1959
1960
Thor-Able III
United States
Douglas /Aerojet
27.4 m
~64 to HEO
1
CCSFS
1959
1959
Thor-Able IV
United States
Douglas /Aerojet
27.2 m
~43 to Heliocentric
1
CCSFS
1960
1960
Thor Agena-A
United States
Douglas /Lockheed
22.7 m
860
16
VAFB
1959
1960
Thor Agena-B
United States
Douglas /Lockheed
26.3 m
1,200
21
VAFB
1962
1965
Thor Agena-D
United States
Douglas /Lockheed
29.3 m
1,150
22
VAFB
1962
1967
Thorad SLV-2G Agena D
United States
Douglas /Lockheed
32.9 m
2,000
30
VAFB
1966
1971
Thorad SLV-2H Agena D
United States
Douglas /Lockheed
34 m
2,000
13
VAFB
1969
1972
Thor-Burner-1 MG-18
United States
Douglas
23 m
770
150-300 to MEO
2
VAFB
1965
1965
Thor-Burner-1 Altair-3
United States
Douglas
~24 m
>73
4
VAFB
1965
1966
Thor-Burner-2
United States
Douglas
22.4 m
250 to MEO
12
VAFB
1966
1971
Thor-Burner-2A
United States
Douglas
23.5 m
300 to MEO
8
VAFB
1971
1976
Thor-Delta
United States
Douglas
31 m
226
45
12
CCSFS
1960
1962
Thor-Delta A
United States
Douglas
31 m
250
68
2
CCSFS
1962
1962
Thor-Delta B
United States
Douglas
31 m
370
68
9
CCSFS
1962
1964
Thor-Delta C
United States
Douglas
27.5 m
81
11
CCSFS
1963
1967
Thor-Delta C1
United States
Douglas
27.5 m
81
2
CCSFS
1966
1969
Thor-Delta D
United States
Douglas
32 m
450
104
2
CCSFS
1964
1965
Thor-Delta E
United States
Douglas
31 m
540
150
6
VAFB, CCSFS
1965
1967
Thor-Delta E1
United States
Douglas
28 m
540
205
17
VAFB, CCSFS
1966
1971
Thor-Delta G
United States
Douglas
30 m
650
2
CCSFS
1966
1967
Thor-Delta J
United States
Douglas
31 m
260
263
1
VAFB
1968
1968
Thor-Delta L
United States
Douglas
35 m
356
300
2
VAFB, CCSFS
1969
1972
Thor-Delta M
United States
Douglas
34 m
356
355
12
CCSFS
1968
1971
Thor-Delta M6
United States
Douglas
32.4 m
454
450
1
CCSFS
1971
1971
Thor-Delta N
United States
Douglas
33 m
900
6
VAFB, CCSFS
1968
1972
Thor-Delta N6
United States
Douglas
33 m
1,600
3
VAFB
1970
1971
Thor-DM21 Able-Star
United States
Douglas /Aerojet
29 m
150
11
CCSFS
1960
1962
Thor-DSV2A Able-Star
United States
Douglas /Aerojet
29 m
150
8
VAFB
1963
1965
Thor-ISS
United States
Douglas /Thiokol
23 m
500 to MEO
5
VAFB
1976
1980
Thor-SLV2A Agena-B
United States
Douglas /Lockheed
31 m
400
2
VAFB
1963
1966
Thor-SLV2A Agena-D
United States
Douglas /Lockheed
29.3 m
1,500
60
VAFB
1963
1968
Tysklon-2
(R-36-O)
Soviet Union
Yuzhmash
32 m
3,350
18
Baikonur
1965
1971
Tsyklon-2A
Soviet Union
Yuzhmash
39.7 m
3,350 [279]
8 [280]
Baikonur
1967
1969
Tsyklon-2M
Soviet Union Ukraine
Yuzhmash
39.7 m
2,820 [281]
106 [282]
Baikonur
1969
2006[282]
Tsyklon-3
Soviet Union Ukraine
Yuzhmash
39.3 m
1,920 [283]
122 [284]
Plesetsk
1977
2009[284]
Unha-2
North Korea
KCST
29.5 m
80
1
Tonghae
2009
2009
Vanguard
United States
Martin
21.9 m
9 [285]
10 (+1)
CCSFS
1957
1959
Vanguard SLV-7
United States
Martin
21.9 m
9 [285]
1
CCSFS
1959
1959
VLS-1
Brazil
AEB , IAE
19.5 m
380 [286]
2 [l] (never reached orbit)
CEA
1997
2003
Volna-O
Russia
Makeyev
14.2 m
100 [287]
1 (+5)[245]