1340-J144

Rocket Motor

NSN 1340-00-008-7791

DEMIL

Shelf Life

UOM

NIIN

Demil:

DEMIL/MLI

Shelf Life:

N/A

UOM:

1 EA

NIIN:

000087791

Product Technical Spec.

Overall Length:

79.000 inches

Size Designation:

5 inch

Specific Usage Design:

Linear demolition charge

Model Number:

Mk 22 mod 0

Motor Propellant Grain Quantity:

Motor Propellant Grain Model Number:

Mk 29 mod 1

Igniter:

Included

Igniter Installation:

Installed

Igniter Model Number:

Mk 127 mod 2

Straight Section Outside Diameter:

5.000 inches

Dod Ammunition Code:

1340-j144

Dot Registration Code:

Ex1988030695

Net Explosive Weight:

43.110001 storage pounds and 43.110001 transportation pounds

Hazardous Material Classification Code:

1.3 department of defense hazard class division

Weight:

120.00 pounds

NSN:

1340-00-008-7791

Item Name:

Engine,rocket,solid Propellant

Cage Code:

99999

Cross Referenced Parts

Part Number

Cage

RNCC

RNVC

RNAAC

Status

MSDS

SADC

Part Number:

657452

Cage Code:

10001

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

LD268042

Cage Code:

10001

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:

86.8 X 12.4 X 9.9

Paclk Weight:

1,910.0000lbs

Item Weight:

Item Dim:

OPI

SPI No.

SPI Rev.

SPC Mkg.

LVL A

LVL B

OPI:

SPI No.:

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:

200.0

WCC:

402

TCC:

SHC:

ACC:

Ammunition

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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.