По вашему запросу найдено документов: 2101
Страница 4 из 211
Evaluation of the initial phase range for transfers in the vicinity of a large space debrisOrbital Maneuvers
Test of the inverse square law through precession of orbitsUsing precession of orbits due to non-Newtonian interaction between two celestial bodies and modern
Orbital Transfers in a Binary Asteroid System Considering Flattening of the Bodies and Solar Radiation Pressure-spherical asteroid system. As an example, we consider the physical and orbital characteristics of the asteroid system
Lunar orbital platform-gatewayLunar orbital platform-gateway
Low orbit spacecraft service planningThe methodical approach for Space Servicing System (SSS) orbit parameters select and flyby planning
Feasibility analysis of large-size space debris de-orbiting from near-Earth orbits with respect to the initial mass of a fuelled SC-collector objects (SDO) to disposal orbit (DO) is given. It is assumed that for such missions a special spacecraft
Orbital volume assessment according to MSCT data in patients with midface traumaPurpose. To acquire additional diagnostic information in patients with orbital trau-ma in order
Large-size space debris flyby in low earth orbits-size space debris (LSSD). These groups are defined according to the proximity of orbital inclinations
Measurements of inferior orbital wall defects according to MSCT data [МЕТОДИКА ОЦЕНКИ ДЕФЕКТОВ НИЖНЕЙ СТЕНКИ ОРБИТЫ ПО ДАННЫМ МУЛЬТИСПИРАЛЬНОЙ КОМПЬЮТЕРНОЙ ТОМОГРАФИИ] tomography (MSCT) in patients with orbital injury in order to obtain additional diagnostic information about
Страница 4 из 211
Фасеты
Партнеры
Индексация
