Purpose of the development: The method is intended for a variety of rapid assessments of the characteristic speed cost multi-turn maneuvers near-Earth space tugs with electric rocket engine. Also, to assess the efficiency of rocket engine electrical perspective, depending on their design parameters.

Recommended application field: In the space industry: the development and evaluation of advanced tugboats to perform interorbital transitions in near-Earth space with the use of electric thrusters. In the space industry: the development and evaluation of advanced tugboats to perform interorbital transitions in near-Earth space with the use of electric thrusters.

Advantages over analogues: The use of the author's technique of using analytic solutions of averaged equations of cosmic movement of the thruster unit to construct quasi-optimal transition trajectory.

The development stage readiness: Tested experimental exploitation order

Description of the development:
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The ability to assess the effectiveness of the use of space tugs with electric thrusters on the spacecraft for various purposes. The ability to optimize the trajectory and the design parameters of spacecraft and propulsion systems.

corresponds technical description
Reguires revision

Possibility of transfer abroad:
Combinated reduction to industrial level
Creation of joint enterprise

Photo

Country Ukraine

For additional information turn to:
E-mail: gal@uintei.kiev.ua