Part Number
Definition:
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).
CAGE Information
| Code | Company |
|---|---|
| 02602 | PRATT & WHITNEY ROCKETDYNE INC. |
Federal Supply Class
Title
ROCKET ENGINES AND COMPONENTS
Inclusions:
INCLUDES ROCKET PRIME MOVERS, LIQUID TYPE, INCLUDING LIQUID JET ASSISTED TAKE OFF (JATO) UNITS, FOR USE IN AIRCRAFT, ROCKETS, AND GUIDED MISSILES; LIQUID PROPELLANTS ENCASED IN CONSUMABLE CONTAINERS, INTENDED FOR INSERTION INTO MISSILE PROPULSION SYSTEMS AS INTEGRAL PARTS.
Exclusions:
EXCLUDES ROCKET MOTORS - SOLID PROPELLANT UNITS (FSC 1337); LIQUID PROPELLANTS PREDETERMINED TO SPECIFIC QUANTITY AND QUALITY, BUT PACKAGED IN REUSABLE CONTAINERS; SOLID PROPELLANT SQUIBS AND CARTRIDGES, WHETHER INTENDED FOR INSERTION INTO LIQUID PROPELLENT SYSTEMS OR NOT (FSC 1337).
Characteristics (Decoded)
| MRC | Requirements Statement | Clear Text Reply |
|---|---|---|
| ZZZV | FSC APPLICATION DATA | LGM118A,PEACEKEEPER MISSLE |
| AXSF | FUEL/OXIDIZER TANK | NOT INCLUDED |
| AXDH | IGNITION TYPE | SPONTANEOUS |
| FEAT | SPECIAL FEATURES | HARDNESS CRITICAL ITEM |
| AXXD | THRUST CHAMBER QUANTITY | 1 |
| AXWY | COOLING SYSTEM TYPE | REGENERATIVE |
| CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |
| AWBF | IGNITER | NOT INCLUDED |
| AXSE | FUEL/OXIDIZER FEED SYSTEM TYPE | PRESSURE |
| AWBS | INTEGRAL THRUST DIRECTION CONTROL METHOD | GIMBLE THRUST VECTOR |