Motor Performance
Reusable Solid Rocket Motor (RSRM) |
|
| Propellant |
PBAN |
| Propellant Segmants: |
4 |
| Average Thrust (vacuum): |
2,600,000 lbf 11,565 kN |
| Chamber Pressure: (Pc) |
918 psia |
| Effective Isp (vacuum): |
267.3 sec |
| Burn Time |
123.6 sec |
| Total Impulse |
321,360,000 lbf-sec 1,429,480 kN-sec |
| Nozzle Area Ratio: |
7.5 |
| Gimbal Capability: |
±8 degrees |
| Motor Loaded Mass: |
1,252,000 lb 567,898 kg |
| Maximum Propellant Load |
1,107,000 lb 502,127 kg |
Motor Size:
Length / Width |
126 ft / 12 ft 38.4 m / 3.7 m |
| Flight Status |
Production |
| Mission(s): |
Space Shuttle |
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