Pegasus-2
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
Hercules solid rocket engine. Used on Pegasus, Taurus. First flight 1989.
Thrust (sl): 97.100 kN (21,829 lbf). Thrust (sl): 9,907 kgf. Chamber Pressure: 58.00 bar. Area Ratio: 65.
Related
- Country
- USA
- Launch Vehicles
- Pegasus, Pegasus/HAPS, Taurus, ARPA Taurus, Pegasus H, Taurus 2210, Taurus 2110, GBI, Taurus 3210, Taurus 3110
- Propellants
- Solid
- Stages
- Pegasus-2
- Agency
- Hercules