UA1207
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
CSD seven-segment solid rocket engine, originally developed in the 1960's for the cancelled MOL project. First flight 1989.
Thrust (sl): 6,410.400 kN (1,441,115 lbf). Thrust (sl): 653,692 kgf. Propellant Formulation: PBAN.
Related
- Country
- USA
- Launch Vehicles
- Titan 3M, Titan 3L2, Titan 3L4, Titan 3C7, Saturn INT-11, Saturn INT-13, Saturn INT-18, Saturn V-ELV, Saturn MLV-V-4(S)-B, Titan 4, Barbarian MM, Titan 5, Titan 402A/IUS, Titan 405A, Titan 403A, Titan 404A, Titan 401A/Centaur
- Propellants
- Solid
- Stages
- UA1207
- Agency
- CSD