Pegasus-1
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. Solid propellant rocket stage. Pegasus stage 1 without the wings and stabilizers.
Thrust (sl): 296.900 kN (66,746 lbf). Thrust (sl): 30,274 kgf. Chamber Pressure: 58.00 bar. Area Ratio: 40.
Related
- Country
- USA
- Launch Vehicles
- Pegasus, Pegasus/HAPS, Taurus, Pegasus H, Hyper X, Taurus 3210, ATK LV, Taurus 3110
- Propellants
- Solid
- Stages
- Pegasus-1
- Agency
- Hercules