Model: 1338-VN40

Rocket Motor Exhaust Nozzle

Properties:

End Application
Amraam aim120a
Dod Ammunition Code
1338-vn40
General Description
Matl. 26 ga (.0179) cold rolled sheet, astm-a366 cadmium plate iaw qq-p-416 class a, type i
NSN
1338-01-174-5707
Part Number
1338-VN40
Description
Nozzle,exhaust,rocket Motor
CAGE

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-VN40 NSN 1338-01-174-5707

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:
162813
UFC:
73220
LTL:
RATING VARIABLE
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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