Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
Pegasus XL-1
Part of Orion 50 Family
Hercules solid rocket engine. Used on Pegasus XL launch vehicle. First flight 1994.

AKA: Orion 50SXL. Status: Active. Number: 28 . Thrust: 589.00 kN (132,412 lbf). Gross mass: 17,934 kg (39,537 lb). Unfuelled mass: 2,886 kg (6,362 lb). Specific impulse: 293 s. Specific impulse sea level: 180 s. Burn time: 73 s. Height: 8.88 m (29.13 ft). Diameter: 1.27 m (4.16 ft).

Thrust (sl): 361.800 kN (81,336 lbf). Thrust (sl): 36,898 kgf. Chamber Pressure: 58.00 bar. Area Ratio: 40.



Country: USA. Launch Vehicles: Pegasus XL, Pegasus XL/HAPS. Propellants: Solid. Stages: Pegasus XL-1. Agency: Hercules.

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
© 1997-2017 Mark Wade - Contact
© / Conditions for Use