RS000200-001-06: ROCKET ENGINE.
The ROCKET ENGINE is a the manufacturer industrial component. Key specifications include igniter: NOT INCLUDED, ignition_type: ELECTRICAL, overall_length: 16.100 INCHES NOMINAL IN, overall_diameter: 9.000 INCHES NOMINAL IN, precious_material: GOLD, fuel/oxidizer_tank: NOT INCLUDED. This part is cataloged in the U.S.
Government catalog under NSN 2845-00-450-4763, 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 | ELECTRICAL |
| overall_length | 16.100 INCHES NOMINAL IN |
| overall_diameter | 9.000 INCHES NOMINAL IN |
| precious_material | GOLD |
| fuel/oxidizer_tank | NOT INCLUDED |
| cooling_system_type | TRANSPIRATION |
| thrust_chamber_quantity | 1 |
| fuel/oxidizer_feed_system_type | PRESSURE |
| integral_thrust_direction_control_method | HINGED THRUST VECTOR |
| NSN | 2845-00-450-4763 |
| THRUST CHAMBER QUANTITY | 1 |
| OVERALL DIAMETER | 9.000 INCHES NOMINAL IN |
| PRECIOUS MATERIAL | GOLD |
| OVERALL LENGTH | 16.100 INCHES NOMINAL IN |
| IGNITER | NOT INCLUDED |
| FUEL/OXIDIZER TANK | NOT INCLUDED |
| COOLING SYSTEM TYPE | TRANSPIRATION |
| FUEL/OXIDIZER FEED SYSTEM TYPE | PRESSURE |
| IGNITION TYPE | ELECTRICAL |
| INTEGRAL THRUST DIRECTION CONTROL METHOD | HINGED THRUST VECTOR |
No substitute or cross-reference records for this part.