FIELD: rocket and space systems. SUBSTANCE: proposed stage contains engine plant, power adapter and units for connection with adjacent stage. Adapter is made in form of two ring supports spaced over length of engine plant and connected by rods. Engine plant is placed inside adapter and is secured rigidly on one of supports, and for axial displacement on other support, for instance, by means of telescopically coupled members. Invention makes it possible to relieve plant form lateral forces and bending moments. EFFECT: improved reliability in operation. 2 cl, 1 dwg
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Authors
Dates
2003-09-27—Published
2001-12-11—Filed