|
Engine Model: Pegasus XL-2. Designer: Hercules. Gross Mass: 4,331 kg (9,548 lb). Empty Mass: 416 kg (917 lb). Propellants: Solid. Thrust(vac): 153.500 kN (34,508 lbf). Thrust(sl): 127.000 kN (28,550 lbf). Isp: 290 sec. Isp (sea level): 240 sec. Burn time: 73 sec. Diameter: 1.27 m (4.16 ft). Length: 3.58 m (11.74 ft). Chambers: 1. Chamber Pressure: 58.00 bar. Area Ratio: 65.00. Country: USA. First Flight: 1994. Last Flight: 2006. Flown: 33.
Engine Model: Pegasus-2. Manufacturer Name: Orion 50. Designer: Hercules. Gross Mass: 3,370 kg (7,420 lb). Empty Mass: 345 kg (760 lb). Propellants: Solid. Thrust(vac): 118.200 kN (26,572 lbf). Thrust(sl): 97.100 kN (21,829 lbf). Isp: 290 sec. Burn time: 74 sec. Diameter: 1.27 m (4.16 ft). Length: 2.65 m (8.69 ft). Chambers: 1. Chamber Pressure: 58.00 bar. Area Ratio: 65.00. Country: USA. First Flight: 1989. Last Flight: 2004. Flown: 19.
Pegasus-2 used on Rocket Stages
Contact us with any corrections, additions, or comments.
Conditions for use of drawings, pictures, or other materials from this site..
To contact astronauts or cosmonauts.
© Mark Wade, 1997 - 2008 except where otherwise noted.
|
|