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Fredouelle, David
This paper examines two examples of testing activities of sub-components of a 300kN methalox first-stage rocket engine developed by Pangea Aerospace, namely, theinjectors and the cryogenic pumps. One of the difficulties of these test campaignsis to e
Externí odkaz:
http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-340724
