| 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 Able III | — | McDonnell Douglas | 08/07/1959 | ✘ | ✘ | 1 | 27.4 | 2.44 | — | — | 668 |
| Thor Agena A | — | McDonnell Douglas | 01/21/1959 | ✘ | ✘ | 15 | 28.0 | 2.44 | 250 | — | 667 |
| Thor Agena D | — | McDonnell Douglas | 06/28/1962 | ✘ | ✘ | 13 | 31.0 | 2.44 | — | — | 667 |
| Thor Burner 1 | — | McDonnell Douglas | 05/20/1965 | ✘ | ✘ | 4 | 23.0 | 2.44 | — | — | 668 |
| Thor Delta C | — | McDonnell Douglas | 11/27/1963 | ✘ | ✘ | 10 | 27.5 | 2.44 | 81 | — | 667 |
| Thor Delta G | — | McDonnell Douglas | 12/14/1966 | ✘ | ✘ | 2 | 30.0 | 2.44 | — | — | 765 |
| Super Heavy Prototype | — | SpaceX | — | ✔ | ✔ | 0 | 70.0 | 9.0 | — | — | — |
| Terran R | — | Relativity Space | — | ✔ | ✔ | 0 | 66.0 | 5.5 | 20000 | — | 9400 |
| Diamant A | — | Société d'étude et de réalisation d'engins balistiques | 11/26/1965 | ✘ | ✘ | 4 | 18.95 | 1.34 | 160 | — | 301 |
| Diamant B | — | Société d'étude et de réalisation d'engins balistiques | 03/10/1970 | ✘ | ✘ | 5 | 23.5 | 1.34 | 160 | — | 396 |
| Thor SLV-2 Agena B | — | McDonnell Douglas | 01/25/1964 | ✘ | ✘ | 3 | 27.2 | 2.44 | 400 | — | 756 |
| Thor SLV-2 Agena D | — | McDonnell Douglas | 05/31/1967 | ✘ | ✘ | 8 | 27.2 | 2.44 | — | — | 756 |
| Thor SLV-2A Agena D | — | McDonnell Douglas | 02/28/1963 | ✘ | ✘ | 61 | 31.0 | 2.44 | — | — | 1571 |
| Titan 23B | — | Lockheed Martin | 08/23/1969 | ✘ | ✘ | 9 | 45.0 | 3.05 | 3000 | — | 2300 |
| Titan 24B | — | Lockheed Martin | 08/12/1971 | ✘ | ✘ | 23 | 45.0 | 3.05 | 3000 | — | 2410 |
| Titan 34B | — | Lockheed Martin | 03/10/1975 | ✘ | ✘ | 11 | 48.0 | 3.05 | 3500 | — | 1997 |
| Black Brant IX | — | Magellan Aerospace Corporation | 03/16/1982 | ✔ | ✘ | 3 | 12.2 | 0.46 | — | — | — |
| Nike Cajun | — | National Aeronautics and Space Administration | 07/06/1956 | ✘ | ✘ | 4 | 7.7 | 0.42 | — | — | 246 |
| Titan II | — | National Aeronautics and Space Administration | 04/08/1964 | ✘ | ✘ | 12 | 33.2 | 3.05 | 3850 | — | 1913 |
| Titan III | — | Lockheed Martin | 02/11/1974 | ✘ | ✘ | 7 | 48.8 | 3.05 | 15400 | — | 12991 |
| Titan 402A IUS | — | Lockheed Martin | 06/14/1989 | ✘ | ✘ | 3 | 54.0 | 3.05 | 21680 | — | 14200 |
| Titan 402B IUS | — | Lockheed Martin | 02/23/1997 | ✘ | ✘ | 5 | 54.0 | 3.05 | 21680 | — | 15000 |
| Titan 403A | — | Lockheed Martin | 03/08/1991 | ✘ | ✘ | 5 | 54.0 | 3.05 | 17700 | — | 14200 |
| Titan 404A | — | Lockheed Martin | 11/28/1992 | ✘ | ✘ | 3 | 54.0 | 3.05 | 17700 | — | 14200 |
| Titan 404B | — | Lockheed Martin | 05/22/1999 | ✘ | ✘ | 3 | 54.0 | 3.05 | 21680 | — | 15000 |