| 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) |
|---|---|---|---|---|---|---|---|---|---|---|---|
| Kinetica 1 | — | CAS Space | 07/27/2022 | ✔ | ✘ | 3 | 30.0 | 2.65 | 2000 | — | 1961 |
| Titan 34B | — | Lockheed Martin | 03/10/1975 | ✘ | ✘ | 11 | 48.0 | 3.05 | 3500 | — | 1997 |
| Thor Delta M | — | McDonnell Douglas | 09/19/1968 | ✘ | ✘ | 12 | 34.0 | 2.44 | 355 | 355 | 2140 |
| Mu-3S | — | Institute of Space and Astronautical Science | 02/17/1980 | ✘ | ✘ | 4 | 23.8 | 1.41 | 300 | — | 2150 |
| Mu-3H | — | Institute of Space and Astronautical Science | 02/19/1977 | ✘ | ✘ | 3 | 23.8 | 1.41 | 300 | — | 2150 |
| Epsilon S | — | Japan Aerospace Exploration Agency | 09/14/2013 | ✔ | ✘ | 0 | 24.4 | 2.5 | — | — | 2158 |
| Minotaur IV | — | Orbital Sciences Corporation | 09/27/2011 | ✔ | ✘ | 1 | 23.9 | 2.35 | 1950 | 0 | 2200 |
| Orion Abort Test Booster | — | National Aeronautics and Space Administration | 07/02/2019 | ✘ | ✘ | 1 | — | 5.5 | — | — | 2200 |
| Minotaur IV | — | Orbital ATK | 09/26/2010 | ✔ | ✘ | 3 | 23.9 | 2.35 | 1735 | 0 | 2200 |
| Minotaur IV | — | Orbital Sciences Corporation | 11/20/2010 | ✔ | ✘ | 1 | 23.9 | 2.35 | 1750 | 0 | 2200 |
| H-IIA | — | Mitsubishi Heavy Industries | 08/29/2001 | ✔ | ✘ | 33 | 53.0 | 4.0 | 10000 | 4100 | 2260 |
| H-IIA | — | Mitsubishi Heavy Industries | 12/18/2006 | ✘ | ✘ | 5 | 53.0 | 4.0 | — | 6000 | 2260 |
| Epsilon | — | Japan Aerospace Exploration Agency | 09/14/2013 | ✔ | ✘ | 6 | 24.4 | 2.5 | — | — | 2271 |
| N-2 | — | Mitsubishi Heavy Industries | 02/11/1981 | ✘ | ✘ | 8 | 35.0 | 2.44 | 2000 | 730 | 2278 |
| Atlas H | — | Convair | 02/09/1983 | ✘ | ✘ | 5 | 27.0 | 3.05 | 3630 | 2255 | 2282 |
| Delta 2914 | — | McDonnell Douglas | 04/13/1974 | ✘ | ✘ | 30 | 35.0 | 2.44 | 724 | — | 2287 |
| Delta 1914 | — | McDonnell Douglas | 11/10/1972 | ✘ | ✘ | 2 | 35.0 | 2.44 | — | — | 2287 |
| Titan 33B | — | Lockheed Martin | 03/21/1971 | ✘ | ✘ | 3 | 45.0 | 3.05 | 3000 | — | 2300 |
| Titan 23B | — | Lockheed Martin | 08/23/1969 | ✘ | ✘ | 9 | 45.0 | 3.05 | 3000 | — | 2300 |
| Tsiklon-2 | — | Yuzhnoye Design Bureau | 08/06/1969 | ✘ | ✘ | 105 | 39.7 | 3.0 | 2820 | — | 2366 |
| Tsiklon-2A | — | Yuzhnoye Design Bureau | 10/27/1967 | ✘ | ✘ | 8 | 39.7 | 3.0 | 3000 | — | 2366 |
| Long March 6C | — | China Aerospace Science and Technology Corporation | — | ✔ | ✘ | 0 | 43.0 | 3.35 | 4500 | — | 2376 |
| Delta 1913 | — | McDonnell Douglas | 06/10/1973 | ✘ | ✘ | 1 | 35.0 | 2.44 | — | — | 2410 |
| Delta 1900 | — | McDonnell Douglas | 12/16/1973 | ✘ | ✘ | 1 | 35.0 | 2.44 | — | — | 2410 |
| Titan 24B | — | Lockheed Martin | 08/12/1971 | ✘ | ✘ | 23 | 45.0 | 3.05 | 3000 | — | 2410 |