Model: 1338-V224

Rocket Motor Exhaust Nozzle

Properties:

Overall Diameter
23.850 inches
End Application
Lgm-30f
Dod Ammunition Code
1338-v224
NSN
1338-01-063-2142
Part Number
1338-V224
Description
Nozzle,exhaust,rocket Motor
CAGE
99999

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 1338-V224 NSN 1338-01-063-2142

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

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
162812
UFC:
73210
LTL:
85.0
LCL:
--
WCC:
778
TCC:
Z
SHC:
9
ACC:
Explosives

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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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