FIELD: aircraft engineering.
SUBSTANCE: claimed system comprises engine plant with spherical oxidizer and fuel tanks, rocket engine, pitch and yaw control channels with angle, linear departure and speed transducers, summation amplifier, servo units, integrators, two logical units, valves and low thrust engines.
EFFECT: higher reliability and efficiency of spacecraft stabilization.
3 dwg
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| MULTI-STAGE ROCKET | 1994 |
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RU2609539C1 |
