1340-22-307-1902

Rocket Motor

1340223071902 223071902

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

1340-22-307-1902 ROCKET MOTOR 1340223071902 223071902

Managed by Denmark
Data Last Changed
January 2024
NATO Update Count
1
NATO Data Quality
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Managed by Denmark Data Last Changed January 2024 NATO Update Count 1 NATO Data Quality NSN 1340-22-307-1902
Denmark (DK) 4. 1340-22-307-1902 Marketplace Restrictions Approved Sources Datasheet Management Open
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1340-22-307-1902 Demil Restrictions 1340-22-307-1902

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1340-22-307-1902 is a Rocket Motor

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