FIELD: aircraft engineering.
SUBSTANCE: spacecraft is brought in atmosphere at maximum aero dynamic effective property. Spacecraft flight current parameters are measured at descent in atmosphere to decrease its speed to appropriate spacecraft atmosphere entry speed. Current magnitudes for spacecraft aerodynamic balancing property are set subject to parameters of spacecraft descent in atmosphere. Said spacecraft aerodynamic balancing property and bank are controlled at isoaltitude section subject to spacecraft flight parameters. Spacecraft is driven from said isoaltitude section to fly in atmosphere at maximum aerodynamic property and zero bank.
EFFECT: decreased maximum full overload at spacecraft sirframe.
2 dwg
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