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) |
---|---|---|---|---|---|---|---|---|---|---|---|
Soyuz 2-1v | — | Progress Rocket Space Center | 12/28/2013 | ✔ | ✘ | 8 | 44.0 | 3.0 | 2850 | — | — |
SS-520 | — | Japan Aerospace Exploration Agency | 02/03/2018 | ✘ | ✘ | 1 | — | 0.5 | 4 | — | — |
Long March 1 | — | China Aerospace Science and Technology Corporation | 04/24/1970 | ✘ | ✘ | 2 | — | — | — | — | — |
Soyuz | — | Progress Rocket Space Center | 05/20/2001 | ✘ | ✘ | 60 | 49.5 | 3.0 | 6450 | — | — |
H-IIA | — | Mitsubishi Heavy Industries | 02/26/2005 | ✘ | ✘ | 3 | 53.0 | 4.0 | — | 4500 | — |
Atlas E/SVS | — | Convair | 12/19/1981 | ✘ | ✘ | 1 | — | — | — | — | — |
Simorgh | — | Iranian Space Agency | 07/27/2017 | ✔ | ✘ | 6 | — | — | — | — | — |
Eris | — | Gilmour Space Technologies | — | ✘ | ✘ | 0 | 25.0 | 2.0 | 305 | — | — |
Delta II | — | United Launch Alliance | 01/10/1998 | ✘ | ✘ | 26 | 38.9 | 2.4 | — | 1840 | — |
Molniya-M | — | Russian Space Forces | 10/04/1965 | ✘ | ✘ | 272 | — | — | — | — | — |
H3 | — | Mitsubishi Heavy Industries | — | ✔ | ✘ | 0 | 63.0 | 5.27 | — | 6500 | — |
Kuaizhou | — | China Aerospace Science and Industry Corporation | 09/25/2013 | ✘ | ✘ | 2 | 11.0 | 1.4 | 0 | 0 | — |
KSLV 2 TLV | — | Korea Aerospace Research Institute | 11/28/2018 | ✘ | ✘ | 1 | — | — | — | — | — |
SSLV | — | Indian Space Research Organization | 08/07/2022 | ✔ | ✘ | 2 | 34.0 | 2.0 | 500 | — | — |