Motor Performance
Solid Rocket Motor Upgrage |
| Propellant |
88% HTBP |
| Propellant Segments: |
3 |
| Average Vacuum Thrust: |
1,700,000 lbf 771,107 kN |
| Chamber Pressure: (Pc) |
1260 psia |
| Effective Isp (vacuum): |
285.6 sec |
| Burn Time |
137.8 sec |
| Total Impulse |
234,260,000 lbf-sec 1,042,040 kN-sec |
| Nozzle Area Ratio: |
16 |
| Gimbal Capability: |
±6 degrees |
| Motor Loaded Mass: |
770,000 lb 349,266 kg |
| Maximum Propellant Load |
688,000 lb 313,000 kg |
Engine Size:
Length / Width |
112 ft / 10.5 ft 34.1 m / 3.2 m |
| Flight Status |
Production |
| Mission(s): |
Titan IVB |
* Engine performance from Alliant web page.
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