NSN 1338-01-121-2630
Rocket Motor Exhaust NozzleDemil:
DEMIL/MLI Shelf Life:
N/A UOM:
1 EA NIIN:
011212630 Pricing & Availability Check
Submit this form for stock availability and pricing.Product Definition Definition of approved item name (AIN): "NOZZLE,EXHAUST,ROCKET MOTOR"
An item designed with a constricting throat section and a divergent section. The constricting throat section compresses the propellant gases and maintains the pressure within the thrust chamber of the rocket motor by limiting the flow of gases. The divergent section controls the expansion of the gases causing increased thrust.
1338-01-121-2630 Spec. NSN part characteristics
MRC:
AGAV
End Application
Pershing ii, surface to surface missile
Cross Reference Parts Part numbers that meet the specification outlined on this page and set by the OEM
Indicates a design/source control reference item
Inidicates part number has been superseded
Identification Item Identification Guide (IIG) and Item Name Code (INC)
INC:
22411 FIIG:
A23900 Concept No.:
App. Key:
A Cond. Code:
2 Status:
A Special material and handling
HMIC:
N PMIC:
A ESD:
ESD:
ADPE:
0 CRITL:
X
Hazmat (HMIC) N
Indicates there is no data in the hmirs and the nsn is in a fsc not generally suspected of containing hazardous materials.
Precious Metals (PMIC) A
Item does not contain precious metal.
ADPE 0
Represents items with no adp components
Criticality X
The item does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application.