PROPULSION SYSTEM OF MANOEUVRING SPACECRAFT ON COMBUSTIBLE FUEL COMPONENTS STORED IN GASEOUS PHASE
	GEORGIEV A F; GOLDFINCHES G A; RIPKA N D; SHAPOVALOV A V
	2024-04-04
专利权人	FEDERAL STATE BUDGETARY EDUCATIONAL (BUDG-Non-standard)
申请日期	2024-04-04
专利号	RU2835045-C1
成果简介	NOVELTY - Invention relates to propulsion systems of spacecrafts, in particular, to providing thermal conditions of engines running on combustible fuel components stored in gaseous phase. Propulsion system comprises a controller, a rocket engine, a unit of nozzles, valves and sensors of gas state parameters. High-pressure cylinders have heat-conducting structure with perforated ribs for efficient heat exchange with rocket engine via pneumatic lines. Temperature sensors are installed in the cylinder. Heat transfer elements with thermal bridges transfer heat from engine to pneumatic system and high pressure cylinders. USE - Cosmonautics. ADVANTAGE - Increased efficiency of heat exchange, reduced weight and complexity of design of propulsion system. 10 cl, 4 dwg
IPC 分类号	B64G-001/40 ; F02K-009/64
国家	俄罗斯
专业领域	信息技术
语种	英语
成果类型	专利
文献类型	科技成果
条目标识符	http://119.78.100.226:8889/handle/3KE4DYBR/17384
专题	中国科学院新疆生态与地理研究所
作者单位	FEDERAL STATE BUDGETARY EDUCATIONAL (BUDG-Non-standard)
推荐引用方式 GB/T 7714	GEORGIEV A F,GOLDFINCHES G A,RIPKA N D,et al. PROPULSION SYSTEM OF MANOEUVRING SPACECRAFT ON COMBUSTIBLE FUEL COMPONENTS STORED IN GASEOUS PHASE. RU2835045-C1[P]. 2024.

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