Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Robert K. Masse"'
Publikováno v:
AIAA Propulsion and Energy 2020 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::33a0ce3b647d7f772b1bcc8548981493
https://doi.org/10.2514/6.2020-3517
https://doi.org/10.2514/6.2020-3517
Autor:
May Allen, Ronald A. Spores, Steven J. Schneider, Robert K. Masse, Thomas E. Vasek, Lynn A. Arrington, Elizabeth Driscoll
Publikováno v:
52nd AIAA/SAE/ASEE Joint Propulsion Conference.
Even as for the GR-1 awaits its first on-orbit demonstration on the planned 2017 launch of NASA's Green Propulsion Infusion Mission (GPIM) program, ongoing efforts continue to advance the technical state-of-the-art through improvements in the perform
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ecc1570036e3a2e84cbc3eac2f4fac1a
https://doi.org/10.2514/6.2016-4577
https://doi.org/10.2514/6.2016-4577
Autor:
Robert K. Masse
Publikováno v:
Physics Essays. 20:383-402
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ca1aaaafb0780d2207e36533a446655d
https://doi.org/10.4006/1.3153413
https://doi.org/10.4006/1.3153413
Publikováno v:
51st AIAA/SAE/ASEE Joint Propulsion Conference.
The NASA Space Technology mission Directorate's (STMD) Green Propellant Infusion Mission (GPIM) Technology Demonstration Mission (TDM) will demonstrate an operational AF-M315E green propellant propulsion system. Aerojet-Rocketdyne is responsible for
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::761f999e23eb400ada20dfb9f214aa2b
https://doi.org/10.2514/6.2015-3753
https://doi.org/10.2514/6.2015-3753
Publikováno v:
49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3f36711ceeeca11ec9dd8728e496e9dc
https://doi.org/10.2514/6.2013-3760
https://doi.org/10.2514/6.2013-3760
Publikováno v:
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
Cold gas propulsion systems offer today’s CubeSats a relatively simple, minimal V propulsion solution. CubeSat mission needs have been identified that would be enhanced or enabled if significant V were available in conjunction with preserving
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3092aa23098012ce7ed5adaa699a4d26
https://doi.org/10.2514/6.2012-4269
https://doi.org/10.2514/6.2012-4269