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pro vyhledávání: '"Jon P. Haas"'
Autor:
Harold D. Beeson, Jon P. Haas, Gary A. Ruff, David B. Hirsch, James H. Williams, Michael D. Pedley
Publikováno v:
SAE Technical Paper Series.
The Orion Crew Exploration Vehicle Module (CM) is being designed to operate in an atmosphere of up to 30% oxygen at a pressure of 10.2 psia for lunar missions. Spacecraft materials selection is based on an upward flammability test conducted in a clos
Publikováno v:
SAE Technical Paper Series.
Detecting and extinguishing fires, along with post-fire atmospheric cleaning and monitoring, are vital components of a spacecraft fire response system. Preliminary efforts focused on the technology evaluation of these systems under realistic conditio
The oxygen compatibility of six polymers used in oxygen service was evaluated after exposure for 48 hours to oxygen pressures ranging from 350 to 6200 kPa (50 to 900 psia), and temperatures ranging from 50 to 250 C (122 to 302 F). Three elastomers we
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a0640f395963a0dfc81bf5fd07692147
https://doi.org/10.1520/stp12488s
https://doi.org/10.1520/stp12488s
Autor:
Jon P. Haas, John Graf, Karen Meyers, Cameron Dunlap, John F. Lewis, Andrew McKernan, Mark M. Weislogel
Publikováno v:
SAE Technical Paper Series.
The International Space Station (ISS) Program requires that there always be a 45 calendar day contingency supply of breathing oxygen. In the early assembly stages, there is only one flight system, the Russian Solid Fuel Oxygen Generator (SFOG), that