Under the Earth conditions you can "execute" a short-term space flight according to the following cyclogram:
"Soyuz" space vehicle insertion into the Earth artificial satellite orbit with full or reduced/shortened in time G-load (up to 4 G, duration up to 540 sec);
Short (60 minutes-long) orbital flight, during which you can verify you adaptation possibilities to weightlessness;
"Soyuz" space vehicle de-orbiting from the Earth artificial satellite orbit with full or reduced/shortened in time G-load (up to the moment of parachute deployment, 6.5 G, duration to 420 sec).
In addition, you can experience a long-term G-load of a desirable value and direction, including simulation of the typical test profiles for fighter - pilots and cosmonauts. You can order testing of different systems (devices) for their reliability and work capacity under G-load conditions.
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