802691

Rocket Motor

NSN 1337-00-908-6852

DEMIL

Shelf Life

UOM

NIIN

Demil:

DEMIL/MLI

Shelf Life:

N/A

UOM:

NIIN:

009086852

Detail Specifications

End Application:

Aim-7e guided missile

Motor Propellant Grain Model Number:

Mk 75 mod 1

Motor Propellant Grain Weight:

91.6 pounds

Criticality Code Justification:

Exwt

Dod Ammunition Code:

1337-v343

Dot Registration Code:

Ex1988060885

Net Explosive Weight:

91.599998 storage pounds and 91.599998 transportation pounds

Gross Weight:

1681.0 pallet pounds and 264.6 shipping container pounds

Dot Hazard Class/division:

1.3

Hazardous Material Classification Code:

1.3 department of defense hazard class division

Quantity Per Shipping Container:

NSN:

1337-00-908-6852

Item Name:

Engine,rocket,solid Propellant

Cage Code:

0MVU3

Manufacturer Part Numbers

Part Number

Cage

RNCC

RNVC

RNAAC

Status

MSDS

SADC

Part Number:

LD624129

Cage Code:

10001

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

2546916

Cage Code:

10001

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

802691

Cage Code:

00405

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

1337-V343

Cage Code:

99999

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:

9,999.9000lbs

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:

WCC:

417

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.