Method for assembling rocket propulsion motor

Power plants – Reaction motor – Method of operation

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60271, 2989001, 277 9, B63H 1100, F16J 900

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053297628

ABSTRACT:
A method for assembling a rocket propulsion motor including a motor case and a nozzle assembly, wherein the assembling is carried out under vacuum so that air can not be presented between a silicon sealant layer and a first O-ring disposed between the motor case and the nozzle assembly, thereby preventing the generation of air passage and air pocket in a silicon sealant layer coated over the assembled portions of the rocket propulsion motor. The silicon sealant is prepared by mixing a silicon sealant material with a setting agent. The mixing is also carried out under vacuum, so as to prevent the sealant from containing air. For venting air from a space defined the silicon sealant layer and the first O-ring under vacuum, a plurality of spacing bolts are used which serve to space the motor case and the nozzle assembly at a predetermined distance.

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A. A. McCool et al., "Space Shuttle Solit Rocket Motor Program, Lessons Learned", AIAA-91-2291, paper presented at 27th AIAA Joint Propulsion Conference, Sacramento, Calif., Jun. 24-26, 1991.
R. Cook et al., "Development of the Case-to-Nozzle Joint for the Space Shuttle Redesigned Solit Rocket Motor", AIAA-89-2773, paper presented at 25th AIAA Joint Propulsion Conference, Monterey, Calif., Jul. 10-2, 1989.
A. J. McDonald, "Return to Flight with the Redesigned Solit Rocket Motor", AIAA-89-2404, paper presented at 25th AIAA Joint Propulsion Conference, Monterey, Calif., Jul. 10-12, 1989.
General Electric Company-Silicon Products Division, Product Data for RTV 31, RTV 60, and RTV 88 Silicon Rubber Compounds 1985, CDS-1868.

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