1340-21-880-2420

Rocket Motor

1340218802420 218802420 605-11700-1 701-241000-001-0 701-241000-000-0

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

1340-21-880-2420 ROCKET MOTOR 1340218802420 218802420

Managed by Canada
NSN Created on 24 Apr 1979
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
1340-21-880-2420 ROCKET MOTOR 1340218802420 218802420 1/1
NSN 1340-21-880-2420 (Generic Image) 1/1

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605-11700-1 701-241000-001-0 701-241000-000-0 A nonairbreathing reaction propulsion device that consists
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887-0249 Practice 2.75 Inch Rocket Warhead DL8140376-1RNCC: 3 | RNVC: 2 | DAC: 6 26 Oct 1981 1340-21-880-2420

1340-21-880-2420 Demil Restrictions 1340-21-880-2420

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

1340-21-880-2420 is a Rocket Motor

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