MK123MOD0

Rocket Motor

NSN 1377-01-246-5280

DEMIL

Shelf Life

UOM

NIIN

Demil:

DEMIL/MLI

Shelf Life:

> 60 mo.

UOM:

1 EA

NIIN:

012465280

Detail Specifications

Overall Length:

18.700 inches

Model Number:

Mk 123 mod 0

Motor Propellant Grain Quantity:

Motor Propellant Grain Model Number:

Not assigned

Motor Propellant Grain Weight:

6.8 pounds

Propellant Inhibitor:

Not included

Igniter:

Included

Igniter Installation:

Installed

Igniter Model Number:

Not assigned

Dod Ammunition Code:

1377-mt30

Dot Registration Code:

Ex1987100984

Net Explosive Weight:

6.75 storage pounds and 6.75 transportation pounds

Gross Weight:

52.5 shipping container pounds

Hazardous Material Classification Code:

1.3 department of defense hazard class division

Quantity Per Shipping Container:

Reference Number Differentiating Characteristics:

As differentiated by unit package quantity and unit package type

NSN:

1377-01-246-5280

Item Name:

Engine,rocket,solid Propellant

Cage Code:

14083

Manufacturer Part Numbers

Part Number

Cage

RNCC

RNVC

RNAAC

Status

MSDS

SADC

Part Number:

MBEU142801

Cage Code:

30003

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

10104523

Cage Code:

A486G

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

1377-MT30

Cage Code:

99999

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

MBEU142801

Cage Code:

30003

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

1377-MT30

Cage Code:

99999

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

10104523

Cage Code:

A486G

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:

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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.