Analysis of performance change according to amount of propellant using mathematical model for ball-type separation bolt

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Publisher
KSAS
Issue Date
2017-10-16
Language
English
Citation

The 2017 Asia-Pacific International Symposium on Aerospace Technology

URI
http://hdl.handle.net/10203/239597
Appears in Collection
AE-Conference Papers(학술회의논문)
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