1337-14-282-4027

Rocket Motor

1337142824027 142824027 RU970-0042C0MBAT 1337-95-000-3154 1337-800-0001

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

1337-14-282-4027 ROCKET MOTOR 1337142824027 142824027

Managed by France
NSN Created on 1 Jan 1971
Data Last Changed
July 2023
NATO Update Count
1
NATO Data Quality
1337-14-282-4027 ROCKET MOTOR 1337142824027 142824027 1/1
NSN 1337-14-282-4027 (Generic Image) 1/1

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1337-14-282-4027 Related Documents Related Documents 1337-14-282-4027 5+ Documents (More...)

RU970-0042C0MBAT 1337-95-000-3154 1337-800-0001 A nonairbreathing reaction propulsion device that consists
RQST NE Updated Every Day 1337-14-282-4027 RQST Updated Every Day 1337-14-282-4027 RQST NE Related Documents
Restrictions 1337-14-282-4027 DEMIL: | DEMILI : | CRITICALITY : | HMIC : | PMIC : | EDC: | ADPEC
| RNVC: 9 | DAC: 9 10 Jun 1982 1337-14-520-8383 https//www.nsnlookup.com /fsg-13/fsc-1337/fr 1337-14-282-4027
Rocket Motor 1337142824027 142824027 Vehicle Explosive Propulsion Units, Solid Fuel; and Components
9 10 Jun 1982 1337-14-520-8383 Rocket Motor 015C080-00RNCC: 3 | RNVC: 2 | DAC: 4 14 Jun 2000 1337-14-282-4027
9 10 Jun 1982 1337-14-520-8383 Rocket Motor 015C080-00RNCC: 3 | RNVC: 2 | DAC: 4 14 Jun 2000 1337-14-282-4027
and Space Vehicle Explosive Propulsion Units, Solid Fuel; and Components (FSC 1337) Jun 2000 1337-14-282-4027

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