Probl. Upr., 2017, Issue 1, Pages 75–85
Control the moving objects and navigation
Determination of spacecraft electric jet engines altitude performance with the methods of experimental design
L. A. Makridenkoab, V. J. Gechaab, N. I. Sidnyaevc, V. V. Onufrievc, S. A. Govorc
a Research and Production Corporation "Space Monitoring Systems, Information & Control and Electromechanical Complexes" named after A. G. Iosifian, Moscow
b "VNIIEM Corporation" JSC, Moscow
c Bauman Moscow State Technical University
The testing technique is suggested, based on the theory of experimental design. The analysis is carried out of flight altitude and speed combinations required for optimal spacecraft control. The relevant values of space environment parameters in front of the satellite are presented. The regression model is obtained of electric jet engine flow characteristics – its parameters dependence on the specific thrust. Attention is paid to multifactorial approach to the experiment performed while managing the propulsion device resources. Illustrated is not successive, but simultaneous change of all relevant factors from one design point to another. Optimal designs of multifactorial experiment are obtained.
spacecraft, engine, experiment planning, flow characteristics, thrust, test, point, plan, equation, observation.
PDF file (813 kB)
L. A. Makridenko, V. J. Gecha, N. I. Sidnyaev, V. V. Onufriev, S. A. Govor, “Determination of spacecraft electric jet engines altitude performance with the methods of experimental design”, Probl. Upr., 2017, no. 1, 75–85
Citation in format AMSBIB
\by L.~A.~Makridenko, V.~J.~Gecha, N.~I.~Sidnyaev, V.~V.~Onufriev, S.~A.~Govor
\paper Determination of spacecraft electric jet engines altitude performance with the methods of experimental design
\jour Probl. Upr.
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