Launch Vehicles

Explore the launch vehicles we use to get to Orbit


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Name Family Manufacturer Maiden Flight Date Active Reusable Launch Count Length (m) Max Diameter (m) LEO Capacity (kg) GTO Capacity (kg) Thrust at Liftoff (kN)
Start Moscow Institute of Thermal Technology 03/28/1995 1 28.9 1.61 645 887
H-IIA Mitsubishi Heavy Industries 08/29/2001 33 53.0 4.0 10000 4100 2260
H-II Mitsubishi Heavy Industries 02/03/1994 7 49.0 4.0 10060 3930
H-IIB Mitsubishi Heavy Industries 09/10/2009 9 56.6 5.2 16500 8000 9000
H-IIA Mitsubishi Heavy Industries 02/04/2002 7 53.0 4.0 5000
H-IIA Mitsubishi Heavy Industries 12/18/2006 5 53.0 4.0 6000 2260
H-IIA Mitsubishi Heavy Industries 02/26/2005 3 53.0 4.0 4500
H3-22 Mitsubishi Heavy Industries 03/07/2023 2 63.0 5.27 4000 7542
N-2 Mitsubishi Heavy Industries 02/11/1981 8 35.0 2.44 2000 730 2278
H-1 Mitsubishi Heavy Industries 08/12/1986 9 42.0 2.44 3200 1100
N-I Mitsubishi Heavy Industries 09/09/1975 7 34.0 2.44 1200 360
H3 Mitsubishi Heavy Industries 0 63.0 5.27 6500
H3-24 Mitsubishi Heavy Industries 0 63.0 5.27 6500 12142
H3-30 Mitsubishi Heavy Industries 0 63.0 5.27 2100 4413
Soyuz Ministry of Defence of the Russian Federation 03/29/2018 4 44.0 3.0 2850
Delta II McDonnell Douglas 05/04/2002 2 40.0 2.44
Delta 2910 McDonnell Douglas 01/22/1978 6 35.0 2.44 2560
Thor Delta E McDonnell Douglas 11/06/1965 6 31.0 2.44 540 150 1452
Thor MG-18 McDonnell Douglas 01/19/1965 2 23.0 2.44 668
Delta II McDonnell Douglas 08/25/1997 1 39.0 2.44 4000
Delta 3924 McDonnell Douglas 10/28/1982 5 36.0 2.44 954 3188
Thor Delta J McDonnell Douglas 07/04/1968 1 31.0 2.44 260 263 1452
Delta 0300 McDonnell Douglas 10/15/1972 3 34.0 2.44 1590
Delta II McDonnell Douglas 06/30/2001 1 39.0 2.44 3020
Delta II McDonnell Douglas 04/13/1990 1 39.0 2.44 1500