Development Technique of Large Composite Tank for Aerospace Vehicle

Zhao, Jin; Yu, Bin; Ma, Tianju; Gu, Sendong

doi:10.1109/icmeas54189.2021.00051

Cited by 1 publication

(1 citation statement)

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“…The performance advantages of cryogenic propellants used in space flight have long been valued and studied by space powers such as the United States. The on-orbit management of cryogenic propellants in the field of aerospace electric propulsion can be divided into five parts according to their functions, including cryogenic storage, surface tension management and supply, cryogenic propellant liquid-gas conversion, highpressure to low-pressure and outlet pressure control, and gas micro-flow regulation [2]. Since the 1950 s, the cryogenic propellant research team represented by NASA team has carried out special research on cryogenic fluid space management (CFM) and zero boil off (ZBO) technology and achieved a series of research results.…”

Section: Introductionmentioning

confidence: 99%

Research on Surface Tension Tank Technology of Aerospace Cryogenic Propellant

Ma,

Yu,

Huang

et al. 2024

Advances in Transdisciplinary Engineering

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This paper briefly introduces the research progress of long-term on-orbit storage and supply technology of cryogenic propellant, analyzes the task characteristics, sorts out the technical difficulties, and puts forward the key technologies. The passive thermal protection technology, active heat transfer technology, Vapor cooled shields technology, thermodynamic vent system technology, pressure control technology, liquid mixing technology and adiabatic support technology are described respectively, which provides a reference for the research of space low temperature storage and supply technology.

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Section: Introductionmentioning

confidence: 99%