Author:
VOROBYEV Alexey Gennadievich,VOROBYEVA Svatlana Sergeevna,ZHANG Lihui,BELIAEV Evgeniy Nikolaevich
Subject
Mechanical Engineering,Aerospace Engineering
Reference22 articles.
1. Complex optimization of propulsion systes’ control system;Kokorin,1983
2. Comparative study of lunar mission requirements and onboard propulsion system performance;Lee;Prog Aerosp Sci,2011
3. Ohminami K, Ogawa H, Uesugi K. Numerical bipropellant thruster simulation with hydrazine and NTO reduced kinetic reaction model. 47th AIAA aerospace sciences meeting including the new horizons forum and aerospace exposition; 2009 Jan 5–8; Orlando, Florida, USA. Reston: AIAA; 2009. p. 452.
4. Ohminami K, Sawai S, Uesugi K, Yamanish N, Koshi M. Hydrazine and di-nitrogen tetroxide combustion model inside film-cooled bipropellant thruster. 45th AIAA/ASME/SAE/ASEE joint propulsion conference & exhibit; 2009 Aug 2–5; Denver, Colorado, USA. Reston: AIAA/ASME/SAE/ASEE; 2009. p. 5044.
5. Rutovskiy NB. Copmplex investigation of parametrs of liquid rocket engine of small thrust using in control system of space vechicle [dissertation]. Moscow: Moscow Aviation Institute; 1973.
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