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1340-01-154-1680

Rocket Motor

1340011541680 011541680 233AS500 1340-J147

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

1340-01-154-1680 ROCKET MOTOR 1340011541680 011541680

Managed by United States
NSN Created on 20 May 1983
Data Last Changed
January 2023
NATO Update Count
16
NATO Data Quality
1340-01-154-1680 ROCKET MOTOR 1340011541680 011541680 1/1
NSN 1340-01-154-1680 (Generic Image) 1/1

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1340-01-154-1680 Related Documents Related Documents 1340-01-154-1680 5+ Documents (More...)

233AS500 1340-J147 A nonairbreathing reaction propulsion device that consists essentially of a thrust
United States (US) 4. 1340-01-154-1680 Marketplace Restrictions Approved Sources Datasheet Management
Request a Quotation from participating marketplace vendors Request Updated Every Day 1340-01-154-1680
Upgrade for $1 a day Upgrade your Account Upgrade 1340-01-245-3945Rocket Motor1340012453945 012453945 233AS500
1340-J147 A nonairbreathing reaction propulsion device that consists essentially of a thrust chamber
Rocket Motor 1340011541680 011541680 Upgrade for $1 a day Upgrade your Account Upgrade 1340-01-
Upgrade for $1 a day Upgrade your Account Upgrade 1340-01-154-1679Rocket Motor1340011541679 011541679 233AS500
1340-J147 A nonairbreathing reaction propulsion device that consists essentially of a thrust chamber
30003 - Naval Air Systems Command Managed (Active) Incomplete Reference RNCC 3 RNVC 1 MEDALS DAC 5 1340-J147
5360-99-000-6582 5360990006582 990006582 is an open coiled spring, wound in various forms and from different shapes and types of materials and finished at the ends, designed to provide resistance to compression forces. excludes springs designed for thermal actuation (springs in which the torsion forces are designed to be counteracted by changes in temperature) and spring, reinforcing, hose.
Upgrade for $1 a day Upgrade your Account Upgrade 1340-01-416-1878Rocket Motor1340014161878 014161878 233AS500

1340-01-154-1680 Demil Restrictions 1340-01-154-1680

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

1340-01-154-1680 is a Rocket Motor that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. 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.

1340-01-154-1680 HTS and ScheduleB Import and Export 1340-01-154-1680

1340-01-154-1680 End Users End Users 1340-01-154-1680

US Army (A901)
Effective Date:
1 Apr 1991
US Navy (NGFF)
Effective Date:
1 Apr 1991
MOE Rule:
WN01
Effective Date:
1 Nov 1998

1340-01-154-1680 Manufacturers Approved Sources 1340-01-154-1680

1340-01-154-1680 Technical Data Datasheet 1340-01-154-1680

Characteristic
Specifications
FIIG
T357-B
Dod Ammunition Code [DDAC]
1340-J147
Dot Registration Code [DTRC]
Ex1987080593
Hazardous Material Classification Code [HMCC]
1.3 Department Of Defense Hazard Class Division
Igniter Installation [AWBG]
Installed
Igniter Model Number [AWBJ]
Mk125-5
Igniter [AWBF]
Included
Model Number [AMWN]
Mk66-2
Motor Propellant Grain Model Number [ATSJ]
Mk 90 Mod 0
Motor Propellant Grain Quantity [ATSG]
1
Motor Propellant Grain Weight [ATSK]
7.1 Pounds
Motor Propellant Material [ATSH]
Ethyl, Cellulose
Net Explosive Weight [EXWT]
7.12205 Storage Pounds And 7.12205 Transportation Pounds
Nominal Burning Time In Seconds [AWBL]
1.10
Nominal Thrust [AWBM]
1516.000 Pounds
Integral Stabilization Method [AWBR]
Fin
Propellant Inhibitor [AWBE]
Included
Quantity Per Shipping Container [QTSC]
4
Reference Number Differentiating Characteristics [ZZZY]
As Differentiated By Unit Pkg Type,Unit Pkg Quantity
Size Designation [ALJP]
2.75 Inch
Overall Length [ABHP]
41.800 Inches Nominal
Weight [WGHT]
13.60 Pounds
Specific Usage Design [ALXZ]
2.75 In. Rocket
Straight Section Outside Diameter [AWBN]
2.750 Inches Nominal

1340-01-154-1680 Management Data Management Data 1340-01-154-1680

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Feb 1987
Department of the Army (DA)
EA
Subscribe
4

Army Army

Materiel Category and Inventory Manager:
D
Single Manager Ammunition
Appropriation and Budget Activity:
K
Ammunition
Management Inventory Segment:
1
Repairable Items(Exclusive of Insurance and Provisioning Items)
This code will be used to identify serviceable or unserviceable items of a durable nature, which when unserviceable normally can be repaired economically by depots or lower echelons of maintenance.
Weapons System / End Item / Homogeneous Group:
Y3
Conventional Ammunition
Folding Fin Aircraft Rocket, 2.75- Inch, All Types
Accounting Requirements:
X
Expendable item.An item of Army property coded with an ARC of X in the AMDF. Expendable items require no formal accountability after issue from a stock record account.Commercial and fabricated items similar to items coded X in the AMDF are considered expendable items.

1340-01-154-1680 Related Items NATO Stock Numbers Related to 1340-01-154-1680

1340-01-154-1680 Freight Data Freight Information 1340-01-154-1680

1340-01-154-1680 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 064300. A Sub NMFC of B. It has a NMFC Description of EXPLOSIVES:AMMO OR CARTRIDGES SUB2. 1340-01-154-1680 is rated as class 85 when transported by Less-Than Truckload (LTL) freight. It has a Uniform Freight Classification (UFC) number of 05980 which rates the freight between FCL and LCL. It has a Water Commodity Code (WCC) of 402 for ocean manifesting and military sealift. 1340-01-154-1680 is classified as Explosive Class B, UN Class 1.2 or 1.3, when transported by water. 1340-01-154-1680 is not a consolidation and does not exceed 84" in any dimension. It should be compatible with a standard 72" Aircraft Cargo Door when transported by air.

1340-01-154-1680 Packaging Data Packaging Data 1340-01-154-1680

Responsible Activity
Packaging Data Source
Primary Inventory Control Activity (PICA)
Packaging Data does not meet current MIL-STD-2073-1E
Storage Environment
Ammunition (Class V; Igloos and Magazines)

Item Pack Level (Unpackaged)

Item Size
Item Weight
Characteristics
Weight/Dimensions Category
Fragility
Item Preservation
--
--
--
Over 10lb
Less than 85G
Special Requirement

Unit Pack Level (Packaged)

Quantity per Pack
Unit Size
Unit Weight
Unit Cube
Preservation Method
Cleaning/Drying
4
51.5" H x 8.0" W x 8.0" L
--
--
--
Special Requirements
Preservation Material
Wrapping Material
Cushioning/Dunnage
Cushioning Thickness
Container
Special Marking
Special Requirement
Special Requirements – see Specific Instructions or Drawings provided
Special Requirements. See Specific Instructions or Drawings Provided
Special Requirements. See Specific Instructions or Drawings Provided
Special requirement – See specific instructions or drawings provided
--

Intermediate Pack Level

Quantity of Unit Packs
Container
--