HT006207

Guided Missil Propulsion Section

NSN 1337-01-365-3799

DEMIL

Shelf Life

UOM

NIIN

Demil:

DEMIL/MLI

Shelf Life:

N/A

UOM:

1 EA

NIIN:

013653799

Product Features

Contains explosives; ddac 1337-vg75; arm 33 porm 4v DC fire 33 porm 4v DC o/a dimen: 7.0 in diameter by 74.0 in l; 157.2 lbs max; airborne installation; forms a portion of the outer case of the missile

Product Technical Spec.

End Application:

Amraam aim-120a g. Missile

Criticality Code Justification:

Feat

Dod Ammunition Code:

1337-vg75

Dot Identification Number:

Un0186

Dot Registration Code:

Ex1994090146a

Net Explosive Weight:

102.6 transportation pounds

Hazardous Material Classification Code:

1.3 department of defense hazard class division

Dot Proper Shipping Name:

Rocket motors

NSN:

1337-01-365-3799

Item Name:

Engine Section,guided Missile

Cage Code:

0MVU3

Cross Referenced Parts

Part Number

Cage

RNCC

RNVC

RNAAC

Status

MSDS

SADC

Part Number:

3820288-104

Cage Code:

82577

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

HT006207

Cage Code:

00405

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

3820288-104

Cage Code:

00405

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

1337-VG75

Cage Code:

99999

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

3820288

Cage Code:

82577

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

3820288-104

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

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Pricing & Availability

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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.