一种微重力环境下低温推进剂被动蒸发量抑制方法和系统
By optimizing the arrangement of multi-layer thermal insulation materials and the flight trajectory design, the problem of controlling the evaporation of cryogenic propellants in a microgravity environment was solved, improving carrying capacity and structural efficiency, and supporting the design of new space transfer and transportation systems.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- BEIJING INST OF ASTRONAUTICAL SYST ENG
- Filing Date
- 2025-09-15
- Publication Date
- 2026-07-17
AI Technical Summary
In existing technologies, cryogenic propellants are easily affected by solar radiation and Earth's infrared radiation in microgravity environments, making it difficult to control evaporation and limiting their long-term application in new space transfer and transportation systems.
Passive evaporation suppression is achieved by using multilayer thermal insulation material (MLI). The arrangement of the multilayer thermal insulation material is optimized by calculating the transfer orbit period, solar position, and Earth shadow model. Combined with flight trajectory design, iterative calculations are performed to control propellant evaporation.
It enables the efficient storage of cryogenic propellants in orbit, improves carrying capacity and structural efficiency, and supports the design and optimization of new space transfer and transportation systems.
Smart Images
Figure CN120964069B_ABST