Back to the Purdue AAE Propulsion main page. Back to the Solid Rockets page.

Alliant Techsystems

Orion 50S AL

Orion 50S AL
Engine statistics
Specification
Applications Pegasus air-launched space booster
Propellants 88% HTPB
Max Thrust 130,500 lb
Avg Thrust 109,140 lb
Burn time 72.4 s
Specific Impulse
Total Impulse 7,893,000 lb-s
Chamber Pressure 847 psia
Weight 29581 lb
Mass Fraction .91
Expansion ratio