| 摘要 |
FIELD: re-entry space vehicles launched into spaces as small payloads (up to 1 ton) by means of light launch vehicles, for example, modified ballistic missiles of submarines. SUBSTANCE: method of operation of vehicle includes injection of vehicle into space at fixed lifetime in space, re-entry and soft touch-down by means of vehicle recovery system, detection of vehicle by means of search systems and delivery of vehicle to base. Season, month, decade when effect of thermodynamic parameters of atmosphere on touch-down dispersion is minimum are forecasted. Depending on scientific problems to be solved, lifetime in space is preset and vehicle is launched into space at such time that its descent should be effected in season and time interval at minimum deviation from rated magnitudes. EFFECT: enhanced efficiency of search and delivery of vehicle to base at minimum deviation of touch-down point from preset magnitudes. 1 dwg |
