A rocket motor structure which includes a head closure and an aft section with a multiplicity of composite tubes mounted therebetween to define a multiplicity of small chambers for providing an overall rocket motor and in which the aft section includes a nozzle structure for the composite tubes and provides attached fins for guiding and stabilizing the structure. Also, the nozzle structure can be provided with an igniter mounted in the nozzle.
Low Cost Antitank Rocket Motor Structure
1983
13 pages
Report
No indication
English
Rocket Engines & Motors , Composite Materials , Ordnance , Patent applications , Rocket engine cases , Solid propellant rocket engines , Fin stabilized ammunition , Antitank missiles , Tubular structures , Composite structures , Mounts , Rocket nozzles , Composite materials , Fiberglass , Graphited materials
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