Part Details | ROCKET ENGINE
2845-01-194-4497 A nonairbreathing reaction propulsion device that consists essentially of an injector, thrust chamber(s) and exhaust nozzle(s), and utilizes liquid fuels and oxidizers at controlled rates from which hot gases are generated by combustion and expanded through a nozzle(s).
Alternate Parts: R023080121, R023080-121, 2845-01-194-4497, 01-194-4497, 2845011944497, 011944497
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | NOV 14, 1984 | 01-194-4497 | 21791 ( ROCKET ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2845-01-194-4497
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| R023080-121 | 02602 | AEROJET ROCKETDYNE OF DE, INC |
Technical Data | NSN 2845-01-194-4497
| Characteristic | Specifications |
|---|---|
| FUEL/OXIDIZER FEED SYSTEM TYPE | PRESSURE |
| FUEL/OXIDIZER TANK | NOT INCLUDED |
| COOLING SYSTEM TYPE | REGENERATIVE |
| IGNITION TYPE | SPONTANEOUS |
| IGNITER | NOT INCLUDED |
| THRUST CHAMBER QUANTITY | 1 |
| INTEGRAL THRUST DIRECTION CONTROL METHOD | GIMBLE THRUST VECTOR |
| SPECIAL FEATURES | NUCLEAR HARDENED |
| NUCLEAR HARDNESS CRITICAL FEATURE | HARDENED |
| FSC APPLICATION DATA | LGM118A,PEACEKEEPER MISSLE |