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-1 Moscow Institute of Thermal Technology 03/25/1993 5 22.7 1.61 632 887
H3-24 Mitsubishi Heavy Industries 0 63.0 5.27 6500 12142
H-IIA Mitsubishi Heavy Industries 08/29/2001 33 53.0 4.0 10000 4100 2260
N-2 Mitsubishi Heavy Industries 02/11/1981 8 35.0 2.44 2000 730 2278
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
H-1 Mitsubishi Heavy Industries 08/12/1986 9 42.0 2.44 3200 1100
H3-30 Mitsubishi Heavy Industries 0 63.0 5.27 2100 4413
H-IIA Mitsubishi Heavy Industries 02/04/2002 7 53.0 4.0 5000
H-IIB Mitsubishi Heavy Industries 09/10/2009 9 56.6 5.2 16500 8000 9000
H3 Mitsubishi Heavy Industries 0 63.0 5.27 6500
H-IIA Mitsubishi Heavy Industries 12/18/2006 5 53.0 4.0 6000 2260
N-I Mitsubishi Heavy Industries 09/09/1975 7 34.0 2.44 1200 360
H-II Mitsubishi Heavy Industries 02/03/1994 7 49.0 4.0 10060 3930
Soyuz Ministry of Defence of the Russian Federation 03/29/2018 4 44.0 3.0 2850
Thor Delta J McDonnell Douglas 07/04/1968 1 31.0 2.44 260 263 1452
Thor Burner 1 McDonnell Douglas 05/20/1965 4 23.0 2.44 668
Delta II McDonnell Douglas 02/07/1999 1 39.0 2.44 3020
Delta 3920-8 McDonnell Douglas 03/24/1989 1 36.0 2.44 3188
Thor Delta E McDonnell Douglas 11/06/1965 6 31.0 2.44 540 150 1452
Delta II McDonnell Douglas 10/24/1998 3 38.4 2.44 2500
Delta 1914 McDonnell Douglas 11/10/1972 2 35.0 2.44 2287
Delta II McDonnell Douglas 02/14/1998 8 39.0 2.44 3020
Delta 2914 McDonnell Douglas 04/13/1974 30 35.0 2.44 724 2287
Thor Able IV McDonnell Douglas 03/11/1960 1 27.2 2.44 668