Zobrazeno 1 - 10
of 20
pro vyhledávání: '"R Joseph Cassady"'
Autor:
Colleen M. Maresse-Reading, James E. Polk, Michael R. LaPointe, Michael G. Houts, James H. Gilland, R. Joseph Cassady, Anita Sengupta, Steven R. Oleson, Derrek Russell, Robert H. Frisbee
Publikováno v:
Energy Conversion and Management. 49:412-435
Nuclear and radioisotope powered electric thrusters are being developed as primary in-space propulsion systems for potential future robotic and piloted space missions. Possible applications for high power nuclear electric propulsion include orbit rai
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cdfbde2753174fc53c4f33e1a58a6407
https://doi.org/10.1016/j.enconman.2007.10.015
https://doi.org/10.1016/j.enconman.2007.10.015
Publikováno v:
2nd International Energy Conversion Engineering Conference.
The increased interest in NASA exploration missions to the outer planets has spurred a revival in interest in applications of radioisotope power to propulsion for the spacecraft. This concept requires a closely coupled systems analysis of the power c
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3378240cda5418184a25676036ba3dfa
https://doi.org/10.2514/6.2004-5614
https://doi.org/10.2514/6.2004-5614
Autor:
R. Joseph Cassady, Ioannis G. Mikellides, Todd Schneider, Todd Peterson, Dale C. Ferguson, G. A. Jongeward, Tom Kerslake, Daniel Homiak, D. Snyder, Andrew Hoskins
Publikováno v:
39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.
The sta:us of development of a Direct Drive Ha!! Thruster System is presented. 13 the first part. a s:udy of the impacts to spacecraft systems and mass benefits of a direct-drive architecture is reviewed. The study initially examines four cases of SP
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::689f00b150ff1e4e13d37bf28acc2c64
https://doi.org/10.2514/6.2003-4726
https://doi.org/10.2514/6.2003-4726
Publikováno v:
36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.
The design and testing of a micro-Pulsed Plasma Thruster (PPT) is presented. Developed for the University of Washington's Dawgstar nanosatellite, the micro-PPT will provide formation keeping, orbit maintenance and attitude control functions to enable
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e4f828956dd9267071b53eb3e1e07ee9
https://doi.org/10.2514/6.2000-3256
https://doi.org/10.2514/6.2000-3256
Autor:
R. Joseph Cassady
Publikováno v:
35th Joint Propulsion Conference and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5f2aec186f14e4be0068533dace0a647
https://doi.org/10.2514/6.1999-2610
https://doi.org/10.2514/6.1999-2610
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