R023080-121: ROCKET ENGINE.
The ROCKET ENGINE is a the manufacturer industrial component. Key specifications include igniter: NOT INCLUDED, ignition_type: SPONTANEOUS, special_features: NUCLEAR HARDENED, fuel/oxidizer_tank: NOT INCLUDED, cooling_system_type: REGENERATIVE, fsc_application_data: LGM118A,PEACEKEEPER MISSLE. This part is cataloged in the U.S.
Government catalog under NSN 2845-01-194-4497, indicating validated use in U.S. government and defense logistics supply chains. Available through authorized enterprise resellers and TPM (Third Party Maintenance) channels.
Verify compatibility with your specific system configuration before ordering.
| igniter | NOT INCLUDED |
| ignition_type | SPONTANEOUS |
| special_features | NUCLEAR HARDENED |
| fuel/oxidizer_tank | NOT INCLUDED |
| cooling_system_type | REGENERATIVE |
| fsc_application_data | LGM118A,PEACEKEEPER MISSLE |
| thrust_chamber_quantity | 1 |
| fuel/oxidizer_feed_system_type | PRESSURE |
| nuclear_hardness_critical_feature | HARDENED |
| integral_thrust_direction_control_method | GIMBLE THRUST VECTOR |
| NSN | 2845-01-194-4497 |
| FSC APPLICATION DATA | LGM118A,PEACEKEEPER MISSLE |
| THRUST CHAMBER QUANTITY | 1 |
| IGNITER | NOT INCLUDED |
| FUEL/OXIDIZER TANK | NOT INCLUDED |
| COOLING SYSTEM TYPE | REGENERATIVE |
| SPECIAL FEATURES | NUCLEAR HARDENED |
| FUEL/OXIDIZER FEED SYSTEM TYPE | PRESSURE |
| NUCLEAR HARDNESS CRITICAL FEATURE | HARDENED |
| IGNITION TYPE | SPONTANEOUS |
| INTEGRAL THRUST DIRECTION CONTROL METHOD | GIMBLE THRUST VECTOR |
No substitute or cross-reference records for this part.