2.5KS18000
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
Multiple-source solid rocket engine. Typical ideal dV=259 m/s; gravity and drag losses = 25 m/s.
Related
- Country
- USA
- Launch Vehicles
- Aerobee RTV-N-8, Aerobee XASR-SC-1, Aerobee RTV-A-1, Aerobee RTV-N-10, Aerobee XASR-SC-2, Aerobee RTV-A-1b, Aerobee RTV-A-1a, Aerobee RTV-N-10b, Aerobee RTV-N-10c, Aerobee Hi, Aerobee AJ10-27, Aerobee RTV-N-10a, Aerobee AJ10-34, Aerobee AJ10-25, Aerobee, Aerobee 100, Aerobee 300, Aerobee 150, Aerobee 150A, Aerobee 300A, Aerobee 150 MI, Aerobee 150A MII
- Propellants
- Solid
- Stages
- 2.5KS18000