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Autor:
Donald C. Morrisey
Publikováno v:
25th Joint Propulsion Conference.
Developed for the Viking mission to Mars in 1975-76, the Viking Lander Capsule terminal descent monopropellant hydrazine rocket engine assemblies represented unique technology for an unusual mission. Intended solely for the purpose of landing an unma
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::213cde5b2371c5e4741000bcea681f42
https://doi.org/10.2514/6.1989-2391
https://doi.org/10.2514/6.1989-2391
