Ion-Plasma Thrusters Thermal Balance Estimation
Journal of Multidisciplinary Engineering Science and Technology (JMEST)
2020
Sergey Kravchenko,
Nikolajs Kuļešovs,
Vladimirs Šestakovs
One of the main problem of the outer
space exploration is the low specific impulse of
spacecraft thrusters. The main limit of the
development of high power and high specific
impulse ion plasma thrusters is their destruction
due to overheating. In this article was developed
thruster losses and efficiency estimation method,
helpful to determine the need in refrigeration
system and main parameters of thruster thermal
balance model
Atslēgas vārdi
Ion-plasma thrusters, thruster electric power looses, thruster heat looses, efficiency, thrust, specific impulse
Hipersaite
http://www.jmest.org/wp-content/uploads/JMESTN42353322.pdf
Kravchenko, S., Kuļešovs, N., Šestakovs, V. Ion-Plasma Thrusters Thermal Balance Estimation. Journal of Multidisciplinary Engineering Science and Technology (JMEST), 2020, Vol. 7, No. 4, 11666.-11674.lpp. e-ISSN 2458-9403.
Publikācijas valoda
English (en)