UA1206
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
CSD solid rocket engine. Used on Titan 34D launch vehicle. First flight 1982.
Thrust (sl): 5,639.500 kN (1,267,810 lbf). Thrust (sl): 575,074 kgf. Propellant Formulation: PBAN.
Related
- Country
- USA
- Launch Vehicles
- Titan 34D/IUS, Titan 34D, Titan 34D/Transtage, Commercial Titan 3
- Propellants
- Solid
- Stages
- UA1206
- Agency
- CSD