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Development of a new MLI for orbital cryogenic propulsion systems -thermal performance under one atmosphere to a vacuum
Development of a new MLI for orbital cryogenic propulsion systems -thermal performance under one atmosphere to a vacuum
2019
Takeshi Miyakita
Kazuya Kitamoto
Kiyoshi Kinefuchi
Masanori Saitoh
Tomoyuki Hirai
Hiroyuki Sugita
Keywords:
Thermal
Aerospace engineering
Atmosphere
Propulsion
Materials science
Computer architecture
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