FIELD: outfitting of solid propellant rocket engines and safety measures taken at outfitting and assembly. SUBSTANCE: stand comprises a device for fixing under which closed chamber 1 is arranged; made on the front bottom of chamber are openings 5 for engine nozzles where projecting inserts 6 are installed; ports 2 are made on the chamber side walls and may be connected to exhaust gas conduits 3. The engine fixing device is made in the form of L-shaped grips 9 mainly of three grips hinge-joined to the front end of chamber, and a grip retainer made in the form of nut 10 installed on the chamber external surface under the grip thrust journals. Carrier ring 11 is installed under the grips ends. EFFECT: enhanced safety. 1 dwg
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Authors
Dates
1996-07-27—Published
1994-03-14—Filed