67E61824-21

Rocket Motor

NSN 1337-00-193-3205

DEMIL

Shelf Life

UOM

NIIN

Demil:

DEMIL/MLI

Shelf Life:

N/A

UOM:

1 EA

NIIN:

001933205

Technical Specifications of NSN

Overall Length:

26.430 inches

End Application:

Lgm-30 missile

Specific Usage Design:

Lgm-30 guided missile

Motor Propellant Grain Weight:

1.4 pounds

Straight Section Outside Diameter:

4.530 inches

Criticality Code Justification:

Exwt

Dod Ammunition Code:

1337-v473

Dot Registration Code:

Ex1988100967

Net Explosive Weight:

2.000000 storage pounds and 2.000000 transportation pounds

Dot Hazard Class/division:

1.2

Hazardous Material Classification Code:

1.2.1 department of defense hazard class division

NSN:

1337-00-193-3205

Item Name:

Engine,rocket,solid Propellant

Cage Code:

98747

Other Related Parts

Part Number

Cage

RNCC

RNVC

RNAAC

Status

MSDS

SADC

Part Number:

1337-V473

Cage Code:

99999

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

67E61824-21

Cage Code:

07868

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Identification

INC

FIIG

Concept No.

App. Key

Cond. Code

Status

INC:

21790

FIIG:

T357-B

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:

Packaging & Shipping

Est. Pack Size

Est. Pack Weight

Est. Item Weight

Est. Item Dim.

Pack Size:

Paclk Weight:

4,500.0000lbs

Item Weight:

Item Dim:

OPI

SPI No.

SPI Rev.

SPC Mkg.

LVL A

LVL B

OPI:

SPI No.:

F004934992

SPI Rev.:

SPC Mkg:

LVL_A:

LVL_B:

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): "Solid Propellant Rocket Engine"

A nonairbreathing reaction propulsion device that consists essentially of a thrust chamber and exhaust nozzle, and that carries its own solid oxidizer-fuel combination from which hot gases are generated by combustion and expanded through a nozzle. See also rocket motor cluster.