Part Number
Definition:
A NONAIRBREATHING REACTION PROPULSION DEVICE THAT CONSISTS ESSENTIALLY OF A THRUST CHAMBER AND EXHAUST NOZZLE, AND THAT CARRIES ITS OWN SOLID OXIDIZER-FUEL COMBINATION FROM WHICH HOT GASES ARE GENERATED BY COMBUSTION AND EXPANDED THROUGH A NOZZLE. SEE ALSO ROCKET MOTOR CLUSTER.
CAGE Information
Code | Company |
---|---|
70272 | ALLIANT TECHSYSTEMS INC. TACTICAL PR |
Federal Supply Class
Title
ROCKETS, ROCKET AMMUNITION AND R
Inclusions:
INCLUDES COMPLETE ROUNDS; EXPLOSIVE COMPONENTS, INCLUDING WARHEADS; PYROTECHNIC ROCKETS; SOLID FUEL JATO UNITS; ROCKET MOTORS (SOLID PROPELLANT UNITS) FOR ROCKETS; COVERS, PROTECTIVE ROCKET WARHEAD; JETTISONABLE ROCKET LAUNCHERS; CONDITIONING KITS AND SETS, CONTROLLED ENVIRONMENT; AND OTHER PECULIAR COMPONENTS WHICH ARE NOT CLASSIFIED ELSEWHERE.
Exclusions:
EXCLUDES NUCLEAR ROCKETS, NUCLEAR WARHEADS; ALL OTHER WARHEADS FOR USE ON OTHER THAN ROCKETS; AND ROCKETS WITH BUILT-IN GUIDING DEVICES.
Characteristics (Decoded)
MRC | Requirements Statement | Clear Text Reply |
---|---|---|
ABHP | OVERALL LENGTH | 50.438 INCHES NOMINAL |
AWBN | STRAIGHT SECTION OUTSIDE DIAMETER | 8.258 INCHES NOMINAL |
AWBG | IGNITER INSTALLATION | INSTALLED |
AWBF | IGNITER | INCLUDED |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | ROCKET MOTOR ASSEMBLY |
DDAC | DOD AMMUNITION CODE | 1340-HA39 |