UA-156
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
CSD solid rocket engine. Tested 1968. Proposed as strap-on booster for Saturn INT-27, Saturn V-25(S)B, Saturn V-25(S)U. Solid propellant rocket stage. 4 Segment version of basic 3-segment UA 156 motor.
Thrust (sl): 8,076.000 kN (1,815,557 lbf). Thrust (sl): 823,538 kgf.
Related
- Country
- USA
- Launch Vehicles
- Saturn INT-27, Saturn V-25(S)B, Saturn V-25(S)U
- Propellants
- Solid
- Stages
- UA-156
- Agency
- CSD