FIELD: rocketry and space engineering. SUBSTANCE: power plant includes rocket engine secured in mount which may perform plane-parallel motion of engine perpendicularly to longitudinal axis of plant. This is achieved due to availability of movable and immovable platforms of mount and servo units which are perpendicular to each other. Servo units are arranged in plane perpendicular to axis of power plant. Engageable with platforms, engine and servo units are groups of rollers which are used to guide motion of engine in direction of axes of servo units. EFFECT: enhanced compensation for disturbances arising due to shift of engine thrust axis from center of mass of spacecraft. 5 cl, 5 dwg
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Authors
Dates
2001-11-20—Published
1997-08-04—Filed