Static orbit communication satellite propulsion system with optimized manufacturability

• Main Authors: ZOU SHUANG, ZHANG LEI, LING MAOYI, TAO CHENG, ZHENG JIANDONG, JING FA, CUI JIATAO
• Format: Patent
• Language: Chinese; English
• Published: 26.03.2019
• Subjects: AIRCRAFT; AVIATION; COSMONAUTICS; PERFORMING OPERATIONS; TRANSPORTING; VEHICLES OR EQUIPMENT THEREFOR

A static orbit communication satellite propulsion system with optimized manufacturability comprises a gas path module, an oxygen path module, a combustion path module and an interconnection pipeline;the gas path module reduces the pressure of high pressure gas provided by a gas cylinder to a desired pressure and provides the decompressed gas to the oxygen path module and the fuel path module; theoxygen path module distributes an oxidizing agent, provided by a storage tank, to a designated engine and a designated thruster; the fuel path module distributes a combustion agent, provided by the storage tank, to the designated engine and the designated thruster; the engine and the thruster generate a thrust force, needed by satellite attitude control and orbit control, by using the oxidizing agent provided by the oxygen path module and the combustion agent provided by the fuel path module; and a communication cabin pipeline in the interconnection pipeline comprehensively considers factors,such as three-cabin dockin