1337-14-489-1721

Rocket Motor

1337144891721 144891721 063V01-200000-0000 0916483Y00 1420AA2019959

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

1337-14-489-1721 ROCKET MOTOR 1337144891721 144891721

Managed by France
NSN Created on 2 Jul 1997
Data Last Changed
July 2023
NATO Update Count
1
NATO Data Quality
1337-14-489-1721 ROCKET MOTOR 1337144891721 144891721 1/1
NSN 1337-14-489-1721 (Generic Image) 1/1

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1337-14-489-1721 Related Documents Related Documents 1337-14-489-1721 5+ Documents (More...)

Space Vehicle Explosive Propulsion Units, Solid Fuel; and Components from France (FR) Jun 1996 1337-14-489-1721
and Space Vehicle Explosive Propulsion Units, Solid Fuel; and Components (FSC 1337) Jun 1996 1337-14-489-1721
5652 https//www.nsnlookup.com /nato/nato-stock-numbers/inc Rocket Motor (INC 21790) Sep 1996 1337-14-489-1721
through a nozzle. see also rocket motor cluster. https//www.nsnlookup.com /fsg-13/fsc-1337/fr 1337-14-489-1721
Rocket Motor 1337144891721 144891721 1337-14-489-1721 1337144891721 144891721 is a nonairbreathing
14 Jun 1978 1337-14-482-2296 Rocket Motor 1337-563-0005RNCC: 6 | RNVC: 9 | DAC: 9 27 Jun 1996 1337-14-489-1721
14 Jun 1978 1337-14-482-2296 Rocket Motor 1337-563-0005RNCC: 6 | RNVC: 9 | DAC: 9 27 Jun 1996 1337-14-489-1721
: 4 5 Jul 1980 1377-14-483-3276 Rocket Motor MBEU170290RNCC: 3 | RNVC: 2 | DAC: 2 5 Sep 1996 1337-14-489-1721

1337-14-489-1721 Demil Restrictions 1337-14-489-1721

DEMIL: | DEMILI: | CRITICALITY: | HMIC: | PMIC: | EDC: | ADPEC:

1337-14-489-1721 is a Rocket Motor

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France (ZF)

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