Document Type : Research Article


1 M. Sc, Faculty of Aerospace Engineering, Amirkabir University of Technology. Tehran., Iran

2 PhD, Faculty of Aerospace Engineering, K. N. Toosi University of Technology, Tehran, Iran



In general, according to the Russian Gost standard, the space propulsion engine system includes injection subsystems, thrust chamber, heat transfer and cooling system, launch system, feeding system, thrust vector control system which due to overlap and penetration The manifolds between the engine reservoirs and the fuel system are usually designed as a pair. In the conducted investigations, in addition to knowing the elements of the circuit and how to arrange the circuit, it also leads to knowing the requirements, goals and main requirements of the system design. Then, based on the studies, the circuit design of the feeding system and the selection of its elements have been done.Considering the cryogenic of the propellants in this project, design considerations for routes and tanks will be more important, and finally, sensitivityanalysis and conceptualdesign considerations have been presented.In this article, the types of feeding systems, Ahead problems and challenges are discussed and finally model of this subsystem will be presented based on the TRL


Main Subjects

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