Zobrazeno 1 - 2
of 2
pro vyhledávání: '"atmospheric entry simulation"'
An assessment is made for the inductively driven plasma wind tunnel PWK3 with the goal to derive relevant mass specific enthalpies for typical Mars and Venus atmospheric entry missions. For this purpose an integral method has been used which links th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::d4012021932ca7b04f57ae87599efe15
Publikováno v:
宇宙航行の力学シンポジウム 平成14年度 = Symposium on Flight Mechanics and Astrodynamics 2002. :29-30
資料番号: AA0045913008