FIELD: transportation.
SUBSTANCE: present invention pertains to systems of controlling processes of separation and dislocation of passive structural elements from acceleration rocket units with a multi-triggered cruise engine unit, designed for putting space objects into desired orbits. The system has a sensor and time setter, unit for switching on the multi-triggered cruise engine unit, unit for switching off the autonomous engine unit, unit for switching on actuating elements of the jettison system, connected to actuating elements, a pressure sensor and a setter in combustion chambers of the cruise and autonomous engine units, a counter and a device for setting the number of starts of the multi-triggered cruise engine unit, an AND gate and comparator units. The interrelationship between these elements allows for, based on comparison of thrust values of both engine units, dislocation of the autonomous engine unit within a minimum time interval after giving the command for switching it off.
EFFECT: increased mass of a space object taken into a desired orbit.
4 dwg
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Authors
Dates
2009-02-20—Published
2006-05-26—Filed