Preliminary design of a small-scale liquid-propellant rocket engine testing platform
Propulsion system testing before mission operation is a fundamental requirement in any project. For both industrial and commercial entities within the space industry, complete system integration into a static test platform for functional and performance testing is an integral step in the system deve...
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| Format: | Others |
| Language: | English |
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Luleå tekniska universitet, Rymdteknik
2019
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| Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-77079 |