Zobrazeno 1 - 8
of 8
pro vyhledávání: '"W. Andrew Hoskins"'
Autor:
Leonard Talerico, W. Andrew Hoskins, Nicole J. Meckel, Randall S. Aadland, Jeffrey M. Monheiser
Publikováno v:
43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
*† ‡ § ¶ The objectives of the NASA’s Evolutionary Xenon Thruster (NEXT) program are to develop a next generation ion propulsion system to Technology Readiness Level 6 and to transfer the NASA technology to industry partners to facilitate the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1e695c0a630001ca4c1aa9aaca750ab1
https://doi.org/10.2514/6.2007-5856
https://doi.org/10.2514/6.2007-5856
Autor:
Jon Polaha, Fred Wilson, Leonard Talerico, Jeff Monheiser, W. Andrew Hoskins, Randall S. Aadland
Publikováno v:
41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
The NASA Evolutionary Xenon Thruster (NEXT) program, led by the NASA Glenn Research Center, is developing the next generation of ion propulsion systems for solar system exploration. The NASA Glenn Research Center led team includes Aerojet, the Jet Pr
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a9cc53f6020a638a89f50ba9df78b676
https://doi.org/10.2514/6.2005-3885
https://doi.org/10.2514/6.2005-3885
Autor:
Nicole J. Meckel, Jonathan Polaha, Jeffrey M. Monheiser, David Q. King, Fred Wilson, Randall S. Aadland, W. Andrew Hoskins
Publikováno v:
39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.
Aerojet General Corporation, Redmond has significantly increased its activity in the development of manufacturable ion propulsion systems in the past 2 years. Aerojet successfully fabricated and demonstrated a 30 cm ion thruster in 1994; completed a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::66218debb7f1b89db2ba7de052270e30
https://doi.org/10.2514/6.2003-4710
https://doi.org/10.2514/6.2003-4710
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
Publikováno v:
35th Joint Propulsion Conference and Exhibit.
A Pulsed Plasma Thruster (PPT) has been developed for use in a technology demonstration flight experiment on the Earth Observing 1 (EO-1) New Millennium Program mission. The thruster replaces the spacecraft pitch axis momentum wheel for control and m
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::07d0553dc8cda97fe10828151d44f821
https://doi.org/10.2514/6.1999-2276
https://doi.org/10.2514/6.1999-2276
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