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NSN 1340-01-017-8410, 1340010178410
NOZZLE,EXHAUST,ROCKET MOTOR

Federal Supply Classification
FSC 1340 - Rockets, Rocket Ammunition and Rocket Components
National Item Identification Number
NIIN 010178410
Codification Country
United States
Item Name Code
INC 22411
Criticality
(N) This item does not have a critical feature such as tolerance, fit restrictions or application. Nuclear hardness properties have not been determined (not valid for input).
Hazardous Material Indicator Code
(N) There is no data in the HMIRS and the NSN is in an FSC not generally suspected of containing hazardous materials.
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DLMS® Summary

National Stock Number 1340-01-017-8410

National Stock Number (NSN) 1340-01-017-8410, or NIIN 010178410, (nozzle,exhaust,rocket motor) was assigned March 14, 1976 in the Federal Logistics Information System (FLIS). This NIIN is Available for Manual Assignment. This NSN does not replace any other NSNs.

There are 2 manufacturer part numbers associated with this NSN. None of the associated part number(s) are considered obsolete. The manufacturer part numbers were originally supplied by one supplier. Today, one supplier is listed as an Active supplier for this NSN. Of the active suppliers, there are no suppliers that are deemed design controlled or valid supply parts.

This part number has not been procured by the US Government in over 5 years.

Based on a planned procurement review by the Primary Inventory Control Activity (PICA) on Apr 02, 1991, this NSN's acquisition method was noted as: Suitable for Competitive Acquisition. (Potential sources shall include dealers/distributors.) This part requires engineering source approval by the design control activity in order to maintain the quality of the part. An alternate source must qualify in accordance with the design control activity's procedures, as approved by the cognizant Government engineering activity. Valid AMCs: 1, 2, 3, 4 and 5.

This NSN is assigned to Item Name Code (INC) 22411. [AN ITEM DESIGNED WITH A CONSTRICTING THROAT SECTION AND A DIVERGENT SECTION. THE CONSTRICTING THROAT SECTION COMPRESSES THE PROPELLANT GASES AND MAINTAINS THE PRESSURE WITHIN THE THRUST CHAMBER OF THE ROCKET MOTOR BY LIMITING THE FLOW OF GASES. THE DIVERGENT SECTION CONTROLS THE EXPANSION OF THE GASES CAUSING INCREASED THRUST.]. This item does not have a critical feature such as tolerance, fit restrictions or application. Nuclear hardness properties have not been determined (not valid for input). There is no data in the HMIRS and the NSN is in an FSC not generally suspected of containing hazardous materials. NSN 1340010178410 does not contain precious metals.

This NSN is associated to Schedule B 9306900080: parts for bombs, grenades, torpedos, mines, and similar munitions of war. The Schedule B End Use is listed as tanks, artillery, missiles, rockets, guns and ammunition. NAICS classification category 332992: small arms ammunition manufacturing.

This information was last updated on .


Technical Characteristics

GENERAL CHARACTERISTICS ITEM DESCRIPTION
(TEXT) RING 1,INSERT 3,4.881 IN. MIN,4.884 IN. MAX OD,3.722 IN. LG

Manufacturer Part Numbers


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