Ballistic researches of perspective technology of group satellites injection into different individual orbits are presented in the article. Methodology for real launch vehicle capabilities determining in case satellites injection into orbits with different altitude and results of analytical and numerical estimation of satellites approaches in group to minimal distances during long time intervals are presented in current article too. The relations received for angular spatial separation of orbit lanes determining and satellites mutual location in case their approach to minimal distances during long time intervals.
group launches, launch vehicle capabilities, satellites spatial separation, angular spatial separation of orbit planes, estimation of satellites approaches, maximal satellites approaches
"Proektno-ballystycheskye yssledovanyia po hruppovыm zapuskam sputnykov v odnom puske raketы nosytelia na raznesennыe bazovыe orbytы" ,
Science and Technology of the Air Force of Ukraine,