Model: 1338011212630

Rocket Motor Exhaust Nozzle

Properties:

End Application
Pershing ii, surface to surface missile
NSN
1338-01-121-2630
Part Number
1338011212630
Description
Nozzle,exhaust,rocket Motor
CAGE
A00AM

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.

Part 1338011212630 NSN 1338-01-121-2630

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
22411
FIIG:
A23900
Concept No.:
App. Key:
A
Cond. Code:
2
Status:
A

Material Classification

Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicators
HMIC
PMIC
ESD/EMI
ENAC
MMAC
CRITL
HMIC:
N
PMIC:
A
ESD:
ESD:
MMAC:
CRITL:
X

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
10.0 X 10.0 X 4.0
Paclk Weight:
0.2000lbs
Item Weight:
0.1000lbs
Item Dim:
008600860017
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
O
SPI No.:
SPI Rev.:
SPC Mkg:
00
LVL_A:
Q
LVL_B:
Q

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Schedule B and Export
  • Schedule B: 9306900060
  • SITC: 89129
  • End Use: Tanks, artillery, missiles, rockets, guns and ammunition
  • NAICS: 336415
  • USDA: 1

Freight Class: Parts for guided missiles

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