Space debris prevention structure of spacecraft
Patent Information
- Authority / Receiving Office
- CN · China
- Current Assignee / Owner
- XI AN JIAOTONG UNIV
- Publication Date
- 2012-06-13
- Estimated Expiration
- Not applicable · inactive patent
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Abstract
Description
Technical field:
[0001] The invention belongs to the field of space debris protection, and relates to a space debris protection structure, in particular to a spacecraft space debris protection structure. Background technique:
[0002] The spacecraft is in an extraordinary space environment during its flight service. The high-speed impact of micrometeorites and space debris seriously threatens the safe operation of near-Earth orbiting spacecraft and the lives of astronauts, and the most important physical feature that threatens the safety of spacecraft is is a mechanical damage effect caused by a hypervelocity impact. Therefore, necessary protective measures must be taken for the spacecraft to ensure its safety in orbit. So far, Whipple protective structure, filled Whipple protective structure, aluminum mesh double-layer protective structure, honeycomb sandwich panel protective structure and multi-layer impact protective structure have been developed. The average impact vel...