1U32329-20

Rocket Motor Exhaust Nozzle

NSN 1338-00-910-7884

DEMIL
Shelf Life
UOM
NIIN
Demil:
DEMIL/MLI
Shelf Life:
UOM:
NIIN:
009107884

Technical Specifications of NSN

Package Nominalheight And Type:
43.00 inches shipping container
Package Nominallength And Type:
29.00 inches shipping container
Package Nominalwidth And Type:
29.00 inches shipping container
Part Name Assigned By Controlling Agency:
Nozzle subassembly, rocket motor
Gross Weight:
224.0 shipping container pounds
Quantity Per Shipping Container:
1
NSN:
1338-00-910-7884
Item Name:
Nozzle,exhaust,rocket Motor
Cage Code:
07703

Other Related Parts

No other part numbers with same form, fit, and function found.

Part Identification

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

Part Materials

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:
--
Paclk Weight:
9,999.9000lbs
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
A
SPI No.:
F009107884
SPI Rev.:
SPC Mkg:
ZZ
LVL_A:
LVL_B:

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
162812
UFC:
73210
LTL:
85.0
LCL:
--
WCC:
427
TCC:
Z
SHC:
9
ACC:
Explosives

  We Guarantee with Every Order

  •   100% Genuine Manufacturers Parts
  •   Every Product thoroughly Inspected
  •   Sales Record Retention of 7 years
  •   Fast Delivery
  •   HAZMAT Certified
  •   Global Shipping

Pricing & Availability

Submit this form for current pricing and availability quote on part number 1u32329-20 and/or cross reference parts.
Part / NSN:
Qty:
Your Email:
Phone:
Ref. / PO #:
Company:

We do not share or sell your information to anyone.
Privacy | Terms

Definition Definition of approved item name (AIN): "Rocket Motor Exhaust Nozzle"

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.

MOE Major Organizational Entities

Entity
DSOR
User:
NADB (NATO AMMUNITION DATA BASE) Nadb (nato Ammunition Data Base)
DSOR:
Import / Export
  • Schedule B: 9306900060
  • SITC: 89129
  • End Use: Tanks, artillery, missiles, rockets, guns and ammunition
  • NAICS: 336415
  • USDA: 1

Classification: Parts for guided missiles


Best-Selling Products A collection of our most popular products