Rupture of a Cryogenic Composite Overwrapped Pressure Vessel Following a High-Speed Particle Impact
A primary spacecraft design consideration is the anticipation and mitigation of the possible damage that might occur in the event of an on-orbit micro-meteoroid or orbital debris (MMOD) particle impact. While considerable effort has been expended in the study of non-pressurized spacecraft components...
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| Format: | Article |
| Language: | English |
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MDPI AG
2018-02-01
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| Series: | Aerospace |
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| Online Access: | http://www.mdpi.com/2226-4310/5/1/20 |