| 摘要 |
FIELD: rocketry and space engineering; small descent spacecraft injected into orbit by ballistic missiles removed from combat duty. ^ SUBSTANCE: proposed descent spacecraft has case, control members for its orientation in space and units for coupling with launch vehicle. Plane of connection of descent spacecraft with launch vehicle coincides with transversal plane of symmetry of case of spacecraft and its diameter coincides in this plane with transversal diameter of launch vehicle. Descent spacecraft case is made in form of body obtained by rotation of oval around its larger axis and said plane of connection with launch vehicle coincides with plane of smaller axis of oval. ^ EFFECT: increased volume of descent spacecraft at limited transversal diameter of launch vehicle. ^ 1 dwg, 1 tbl |
