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1340-01-114-2313

Rocket Motor

1340011142313 011142313 2847573 1340-J143

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. View more Rocket Motor

1340-01-114-2313 ROCKET MOTOR 1340011142313 011142313

Managed by United States
NSN Created on 15 Jun 1981
Data Last Changed
January 2023
NATO Update Count
9
NATO Data Quality
1340-01-114-2313 ROCKET MOTOR 1340011142313 011142313 1/1
NSN 1340-01-114-2313 (Generic Image) 1/1

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1340-01-114-2313 Related Documents Related Documents 1340-01-114-2313 5+ Documents (More...)

2847573 1340-J143 A nonairbreathing reaction propulsion device that consists essentially of a thrust
United States (US) 4. 1340-01-114-2313 Marketplace Restrictions Approved Sources Datasheet Management
DEMIL: G | DEMILI : 1 | CRITICALITY : X | HMIC : N | PMIC : A | EDC: | ADPEC : 0 1340-01-114-2313
a day Upgrade your Account Upgrade 1340-01-116-7799Rocket Motor1340011167799 011167799 DL5546210 1340-J143
a day Upgrade your Account Upgrade 1340-00-187-5104Rocket Motor1340001875104 001875104 DL2847573 1340-J143
NumberManufacturerStatusDL2847573 10001 - Navair And Navsea Managed Original (Active) Primary Buy RNCC 3 RNVC 2 DAC 1 1340-J143
a day Upgrade your Account Upgrade 1340-00-187-5104Rocket Motor1340001875104 001875104 DL2847573 1340-J143
NumberManufacturerStatusDL2847573 10001 - Navair And Navsea Managed Original (Active) Primary Buy RNCC 3 RNVC 2 DAC 1 1340-J143
your Account Upgrade 1340-01-118-2838Rocket Motor1340011182838 011182838 525-174-0129 DL5546211 1340-J143
a day Upgrade your Account Upgrade 1340-00-187-5104Rocket Motor1340001875104 001875104 DL2847573 1340-J143
NumberManufacturerStatusDL2847573 10001 - Navair And Navsea Managed Original (Active) Primary Buy RNCC 3 RNVC 2 DAC 1 1340-J143
-5310 RQST https https//www.nsnlookup.com /cage https//www.nsnlookup.com /fsg-13/fsc-1340/us 1340-01-114-2313
Rocket Motor 1340011142313 011142313,2847573 Inner Tube 2610-66-018-8743Vehicular Pneumatic Tire
Inner Tube2610660188743 660188743 12.00-20 TR175A/90G13 2847573 TR175A/90G13 Z3551 - Goodyear & Dunlop

1340-01-114-2313 Demil Restrictions 1340-01-114-2313

DEMIL: G | DEMILI: 1 | CRITICALITY: X | HMIC: N | PMIC: A | EDC: | ADPEC: 0

1340-01-114-2313 is a Rocket Motor that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. Demilitarization of this item has been confirmed and is not currently subject to changes. This item is Ammunition or Explosive and is a US Munitions List or Commerce Control List Item where demilitarization is required. This item is not suspected to be hazardous. This item does not contain a precious metal.

1340-01-114-2313 HTS and ScheduleB Import and Export 1340-01-114-2313

1340-01-114-2313 End Users End Users 1340-01-114-2313

MOE Rule:
WN01
Effective Date:
1 Nov 1998

1340-01-114-2313 Manufacturers Approved Sources 1340-01-114-2313

1340-01-114-2313 Technical Data Datasheet 1340-01-114-2313

Characteristic
Specifications
FIIG
T357-B
Dod Ammunition Code [DDAC]
1340-J143
Cable Assembly Connector Type [AWBK]
Jack Plug
Cable Assembly Model Number [ATSP]
Not Assigned
Igniter Model Number [AWBJ]
Mk 275 Mod 1
Igniter Installation [AWBG]
Installed
Igniter [AWBF]
Included
Model Number [AMWN]
Mk 22 Mod 3
Motor Propellant Grain Model Number [ATSJ]
N5
Motor Propellant Grain Quantity [ATSG]
1
Motor Propellant Grain Weight [ATSK]
45.0 Pounds
Motor Propellant Material [ATSH]
Solventless Double Base Propellant
Nominal Burning Time In Seconds [AWBL]
2.50
Nominal Thrust [AWBM]
3700.000 Pounds
Propellant Accommodation Type [AWBH]
Internal Star, Extruded
Propellant Inhibitor [AWBE]
Included
Reference Number Differentiating Characteristics [ZZZY]
As Differentiated By Unit Package Quantity,Unit Package Type,Motor Propellant Grain Model Number,Motor Propellant Grain Weight,Nominal Thrust
Resonance Rod [AWBQ]
Not Included
Size Designation [ALJP]
5 Inch
Overall Length [ABHP]
76.000 Inches Nominal
Weight [WGHT]
120.000 Pounds
Specific Launcher For Which Designed [AWBT]
Demolition Kit,M125,M126
Specific Usage Design [ALXZ]
Linear Demolition Charge
Straight Section Outside Diameter [AWBN]
5.000 Inches Nominal

1340-01-114-2313 Related Items NATO Stock Numbers Related to 1340-01-114-2313

1340-01-114-2313 Freight Data Freight Information 1340-01-114-2313

1340-01-114-2313 has freight characteristics.. 1340-01-114-2313 has a variance between NMFC and UFC when transported by rail and the description should be consulted.