SRM-1
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
Credit: NASA
CSD solid rocket engine. Used in TOS; IUS-1 on Shuttle, Titan 34D. Known by manufacturer as Orbus 21. Propellant: 86% solids made up of HTPB UTP-19360A. Shape: cylindrical. First flight 1982. Solid propellant rocket stage. IUS-2 stage with simplified electronics.
Thrust (sl): 70.500 kN (15,849 lbf). Thrust (sl): 7,191 kgf. Chamber Pressure: 58.00 bar. Area Ratio: 64. Propellant Formulation: HTPB.
Related
- Country
- USA
- Launch Vehicles
- Titan 34D/IUS, Titan 34D, Titan 402A/IUS, Commercial Titan 3, Titan 405A, Athena-1, Titan 402B/IUS, Athena-2, Athena-3
- Propellants
- Solid
- Stages
- SRM-1
- Agency
- CSD