FIELD: aviation; astronautics.
SUBSTANCE: invention relates to aerospace engineering. Electric air launch system of a space rocket contains a base with a control system for the launch system and batteries for its power supply. Base is made in the form of a non-rotating ring. To the ring, support rods are attached at their own ends, containing at the other ends of the heel of the support rods interacting with catapults containing the catapult rotors, stators of which are placed on the supporting bars, and heels of catapults for supporting the space rocket. Upper rotating ring with attached blades is supported by means of a magnetic suspension system, the upper part of a nonrotating ring with the electric drive of the upper rotating ring. Lower rotating ring with attached blades is supported by the magnetic suspension system by the lower part of the non-rotating ring. Power supply of the base electrical units is carried out by means of a ground power supply.
EFFECT: increase the reliability, economy and environmental safety of the launch system.
1 cl, 7 dwg
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Authors
Dates
2018-06-19—Published
2017-04-28—Filed