Model: 10230201-504

Rocket Motor Exhaust Nozzle

Properties:

End Application
1410-01-205-7066
Test Data Document
18876-10230201-504 drawing (this is the basic governing drawing, such as a contractor drawing, original equipment manufacturer drawing, etc.; excludes any specification, standard or other document that may be referenced in a basic governing drawing)
General Description
18.076 in l; 11.067 in d; beveled to 5.687 in d on thrust end
NSN
1338-01-234-7485
Part Number
10230201-504
Description
Nozzle,exhaust,rocket Motor
CAGE
18876

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 10230201-504 NSN 1338-01-234-7485

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:
N

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
18.0 X 18.0 X 24.6
Paclk Weight:
44.9000lbs
Item Weight:
13.6000lbs
Item Dim:
018101110111
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
M
SPI No.:
SPI Rev.:
SPC Mkg:
00
LVL_A:
Q
LVL_B:
Q

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
162812
UFC:
73210
LTL:
85.0
LCL:
85.0
WCC:
686
TCC:
Z
SHC:
9
ACC:
Equipment for Aircraft

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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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