1337-VG78

Guided Missil Propulsion Section

NSN 1337-01-376-3185

DEMIL

Shelf Life

UOM

NIIN

Demil:

DEMIL/MLI

Shelf Life:

N/A

UOM:

1 EA

NIIN:

013763185

Detail Specifications

End Application:

Aim-120 amraam

Criticality Code Justification:

Agav

Dod Ammunition Code:

1337-vg78

Dot Identification Number:

Un0186

Dot Registration Code:

Ex1994090146

Hazardous Material Classification Code:

1.3 department of defense hazard class division

Dot Proper Shipping Name:

Rocket motors

Type/model Designation:

Wpu-6/b

NSN:

1337-01-376-3185

Item Name:

Engine Section,guided Missile

Cage Code:

99999

Manufacturer Part Numbers

Part Number

Cage

RNCC

RNVC

RNAAC

Status

MSDS

SADC

Part Number:

3820289-102

Cage Code:

15090

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

HT006559

Cage Code:

00405

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

3820289-100

Cage Code:

82577

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

HT006559

Cage Code:

0MVU3

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Identification

INC

FIIG

Concept No.

App. Key

Cond. Code

Status

INC:

61617

FIIG:

A560Y0

Concept No.:

App. Key:

Cond. Code:

Status:

Part Materials

Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicators

HMIC

PMIC

ESD/EMI

ENAC

MMAC

CRITL

HMIC:

PMIC:

ESD:

MMAC:

CRITL:

Freight Classification

NMFC

UFC

LTL

LCL

WCC

TCC

SHC

ACC

NMFC:

064300

UFC:

05980

LTL:

200.0

LCL:

WCC:

427

TCC:

SHC:

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 1337-vg78 and/or cross reference parts.

Definition Definition of approved item name (AIN): "Guided Missile Engine Section"

An item consisting of one or more rocket engine or rocket motor and a portion of the outer aerodynamic shell or skin of a guided missile (as modified) or a bomb, guided (as modified), designed to provide all or part of the thrust required to power the weapon's flight. Must include either moveable control surface(s), steering jets, jet vane(s), or a combination of these, unless equipped with an articulated nozzle. May also have stabilizing fins, but only in combination with other controlling surfaces, jets, or the like. It is designed to mate with other guided missile section(s) or guided bomb sections. Addition of this to a bomb, guided (as modified) creates a guided missile (as modified). Excludes rocket motor; rocket motor cluster; and guided missile main assemblage.