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 A Transtage | |
| Manufacturer | Martin Marietta |
|---|---|
| Country of origin | United States |
| Used on | Titan III |
| General characteristics | |
| Height | 4.57 meters (15.0 ft) |
| Diameter | 3.05 meters (10.0 ft) |
| Gross mass | 12,247 kilograms (27,000 lb) |
| Engine details | |
| Powered by | 2 AJ10-138 |
| Maximum thrust | 8,000 lbf (36 kN) each[1] |
| Specific impulse | 311 seconds (3.05 km/s) |
| Burn time | 440 seconds |
| Propellant | Aerozine 50 / N2O4 |
Transtage, given the United States Air Force designation SSB-10A, was an American upper stage used on Titan III rockets, developed by Martin Marietta and Aerojet.
- ^ Wade, Mark. "AJ10-138". Encyclopedia Astronautica. Archived from the original on December 28, 2016. Retrieved 2019-07-24.
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