System for storing, regasifying and feeding working fluid to propulsion systems of spacecraft, has cylinder high-pressure vessel whose cavity with cryogenic filling is connected to tank with liquefied working fluid
	DOVGYALLO A I; UGLANOV D A; SHIMANOVA A B
	2023-09-04
专利权人	UNIV SAMARA NAT RES (UYSA-Non-standard)
申请日期	2023-09-04
专利号	RU2023123034-A
成果简介	NOVELTY - The system has a shut-off element with a filling and emptying line connected to an inner vessel of a cylinder with cryogenic filling, and containing a Teflon(RTM: PTFE) bag. A supply line of liquefied working fluid is connected to a gasification line of working fluid. An inner vessel of the cylinder is provided with the cryogenic filling through a filling and emptying line. A shut-off element is connected to the gasification line of the working fluid, which is connected to an inlet of a heat exchange surface of a heat exchanger-gasifier. A cavity of the high-pressure vessel of the cylinder with cryogenic filling is connected through shut-off devices to the working fluid supply line to a propulsion system of a spacecraft. A cavity of the high-pressure vessel of the cylinder with the cryogenic filling is connected to the tank with liquefied working fluid through a working fluid return line through the shut-off devices and a heat exchanger. USE - System for storing, regasifying and feeding working fluid to propulsion systems of a spacecraft.
IPC 分类号	B64D-037/00 ; F17C-007/00
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/20537
专题	中国科学院新疆生态与地理研究所
作者单位	UNIV SAMARA NAT RES (UYSA-Non-standard)
推荐引用方式 GB/T 7714	DOVGYALLO A I,UGLANOV D A,SHIMANOVA A B. System for storing, regasifying and feeding working fluid to propulsion systems of spacecraft, has cylinder high-pressure vessel whose cavity with cryogenic filling is connected to tank with liquefied working fluid. RU2023123034-A[P]. 2023.

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