| 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) |
|---|---|---|---|---|---|---|---|---|---|---|---|
| Thor Delta E1 | — | McDonnell Douglas | 07/01/1966 | ✘ | ✘ | 17 | 28.0 | 2.44 | 540 | 150 | 1450 |
| Thor Delta E | — | McDonnell Douglas | 11/06/1965 | ✘ | ✘ | 6 | 31.0 | 2.44 | 540 | 150 | 1452 |
| Thor Delta D | — | McDonnell Douglas | 08/19/1964 | ✘ | ✘ | 2 | 32.0 | 2.44 | 450 | 104 | 1571 |
| Thor Delta C1 | — | McDonnell Douglas | 05/25/1966 | ✘ | ✘ | 3 | 27.5 | 2.44 | 81 | — | 756 |
| Thor Delta C | — | McDonnell Douglas | 11/27/1963 | ✘ | ✘ | 10 | 27.5 | 2.44 | 81 | — | 667 |
| Thor Delta B | — | McDonnell Douglas | 12/13/1962 | ✘ | ✘ | 9 | 31.0 | 2.44 | 370 | 68 | 667 |
| Thor Delta A | — | McDonnell Douglas | 10/02/1962 | ✘ | ✘ | 2 | 31.0 | 2.44 | 250 | 68 | 667 |
| Thor Delta | — | McDonnell Douglas | 05/13/1960 | ✘ | ✘ | 9 | 31.0 | 2.44 | 226 | — | 667 |
| Thor Burner 2A | — | McDonnell Douglas | 10/14/1971 | ✘ | ✘ | 8 | 23.0 | 2.44 | — | — | 750 |
| Thor Burner 2 | — | McDonnell Douglas | 09/16/1966 | ✘ | ✘ | 12 | 22.4 | 2.44 | — | — | 750 |
| Thor Burner 1 | — | McDonnell Douglas | 05/20/1965 | ✘ | ✘ | 4 | 23.0 | 2.44 | — | — | 668 |
| Thor Agena D | — | McDonnell Douglas | 06/28/1962 | ✘ | ✘ | 13 | 31.0 | 2.44 | — | — | 667 |
| Thor Agena A | — | McDonnell Douglas | 01/21/1959 | ✘ | ✘ | 15 | 28.0 | 2.44 | 250 | — | 667 |
| Thorad SLV-2H Agena D | — | McDonnell Douglas | 06/05/1969 | ✘ | ✘ | 13 | 34.0 | 2.44 | — | — | 1571 |
| Thorad SLV-2G Agena D | — | McDonnell Douglas | 08/09/1966 | ✘ | ✘ | 30 | 32.9 | 2.44 | — | — | 1444 |
| Thor Able IV | — | McDonnell Douglas | 03/11/1960 | ✘ | ✘ | 1 | 27.2 | 2.44 | — | — | 668 |
| Thor Able III | — | McDonnell Douglas | 08/07/1959 | ✘ | ✘ | 1 | 27.4 | 2.44 | — | — | 668 |
| Thor Able II | — | McDonnell Douglas | 01/23/1959 | ✘ | ✘ | 2 | 27.3 | 2.44 | — | — | 668 |
| Thor Able I | — | McDonnell Douglas | 04/24/1958 | ✘ | ✘ | 3 | 30.0 | 2.44 | 120 | — | 667 |
| Terran R | — | Relativity Space | — | ✔ | ✔ | 0 | 66.0 | 5.5 | 20000 | — | 9400 |
| Terran 1 | — | Relativity Space | 03/23/2023 | ✔ | ✘ | 1 | 35.0 | 2.3 | 1479 | — | 920 |
| Super Heavy Prototype | — | SpaceX | — | ✔ | ✔ | 0 | 70.0 | 9.0 | — | — | — |
| Strela | — | Khrunichev State Research and Production Space Center | 12/05/2003 | ✘ | ✘ | 3 | — | — | — | — | — |
| Start-1.2 | — | Moscow Institute of Thermal Technology | 03/04/1997 | ✘ | ✘ | 1 | 22.7 | 1.8 | — | — | 500 |
| Start-1 | — | Moscow Institute of Thermal Technology | 03/25/1993 | ✘ | ✘ | 5 | 22.7 | 1.61 | 632 | — | 887 |