UA1205
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
CSD solid rocket engine. Out of production. Strap-on boosters for Titan 3C, 3D, 3E. Proposed for advanced Saturn IB versions. First flight 1965.
Thrust (sl): 5,293.300 kN (1,189,981 lbf). Thrust (sl): 539,775 kgf. Propellant Formulation: PBAN.
Related
- Country
- USA
- Launch Vehicles
- Titan IIIC, Saturn MLV-V-4(S), Saturn MLV-V-4(S)-A, Saturn IB-D, Saturn INT-12, Saturn INT-16, Titan IIID, Titan 23C, Titan IIIE
- Propellants
- Solid
- Stages
- UA1205
- Agency
- CSD