Analysis of the Technical Implementation Options for Launching a Carrier For Output of Micro Satellites to LEO from an Aircraft Platform (LatLaunch project)

Rīgas Tehniskās universitātes 61. starptautiskā zinātniskā konference 2020
Sergey Kravchenko, Natalia Panova, Nikolajs Kuļešovs, Ilmārs Blumbergs, Vladimirs Šestakovs

This is article in where we trying to solve the problem of increasing specific impulse and thrust of spacecraft electric thrusters by preventing their structure destruction due to overheating in a way of refrigeration their plasma contacting parts

Keywords
Ion thrusters, plasma thrusters, looses, heat looses, efficiency, thrust, specific impulse

Kravchenko, S., Panova, N., Kuļešovs, N., Blumbergs, I., Šestakovs, V. Analysis of the Technical Implementation Options for Launching a Carrier For Output of Micro Satellites to LEO from an Aircraft Platform (LatLaunch project). In: Rīgas Tehniskās universitātes 61. starptautiskā zinātniskā konference, Latvia, Rīga, 15-16 October, 2020. Rīga: RTU Press, 2020, pp.16-17.

Publication language
English (en)