FIELD: space engineering and rocketry; engine plants of cryogenic stages and space vehicles. SUBSTANCE: system includes spherical thin-walled main tanks arranged over circumference and additional tanks similar to main ones. Main tanks are provided with spacers fitted between them. Each spacer is truncated by three planes: two planes are located at similar angular distance from plane passing through center of spacer and longitudinal axis of tankage and third plane is parallel to axis of tankage. Two first contours of spacers are connected with main tanks and third contour is connected to additional tanks. EFFECT: enhanced efficiency. 5 cl, 5 dwg
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Authors
Dates
1997-10-10—Published
1996-01-10—Filed