... vehicle insertion into the Earth artificial satellite orbit with full or reduced ... Soyuz" space vehicle de-orbiting from the Earth artificial satellite orbit with full ...
... of two or three persons to near-earthorbit up to 450 km high, active docking to ... liquid and gaseous working bodies to near-earthorbit up to 450 km high, active (or ...
... Realization of manned flights to near-earthorbits on basis of modernized manned and cargo spacecrafts for the duration period ... Realization of manned flights to near-earthorbits for the period of up to 45-60 days (for the crew of 3 or 2 persons ...
... to the following profiles: take-off, Earthorbit insertion, de-orbiting and descent ... a flight to the Earth, flight on an interplanetary elliptic orbit, braking burn for ...
... Chest-to-Spine" direction, 8 G, peak for 40 seconds; . Typical profile "Insertion of the space vehicle into the Earthorbit". ... The "Soyuz" rocket launcher profile of insertion in the Earthorbit: . Typical "descent" profile; . ...
... i - defines the orientation of the orbit with respect to the Earth's equator . ... where the low point, perigee, of the orbit is with respect to the Earth's surface ... and descending orbit locations with respect to the Earth's equatorial plane ...