Zobrazeno 1 - 6
of 6
pro vyhledávání: '"T. W. Macie"'
Publikováno v:
Journal of Spacecraft and Rockets. 7:968-976
Solar electric propulsion system performance consisting of thrustors with thrust vector aligning actuators, switching network and flight type power conditioner
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1e22ffed968f1895dd38244d33d3e3e6
https://doi.org/10.2514/3.30079
https://doi.org/10.2514/3.30079
Autor:
T. W. Macie, M. L. Macmedan
Publikováno v:
11th Electric Propulsion Conference.
A concept for automatic control of the thrust subsystem has been developed by JPL and participating NASA Centers. This paper reports on progress in implementing the concept at JPL. Control of the Thrust Subsystem (TSS) is performed by the spacecraft
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::503a5aea785d7a9c269cde18dcb15c9f
https://doi.org/10.2514/6.1975-381
https://doi.org/10.2514/6.1975-381
Publikováno v:
11th Electric Propulsion Conference.
An investigation has been conducted in order to assess the impact of magnetic fields generated by the propulsion module upon the scientific instrumentation of the spacecraft as proposed for the mission to comet Encke. It was found that dc magnetic fi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8664ebece16322e2f66951707b85bddc
https://doi.org/10.2514/6.1975-373
https://doi.org/10.2514/6.1975-373
Autor:
Ε. N. Costogue, T. W. Macie
Publikováno v:
1971 IEEE Power Electronics Specialists Conference.
The successful integration of a light-weight, high-efficiency power conditioning (PC) unit with an electron bombardment ion thruster using a hollow cathode at JPL has been reported recently. This paper summarizes the presently conceived requirements
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b52fb859cee34f914f3e8ee89dd2635c
https://doi.org/10.1109/pesc.1971.7069131
https://doi.org/10.1109/pesc.1971.7069131
Autor:
T. W. Macie, T. D. Masek
Publikováno v:
8th Electric Propulsion Conference.
Achievements in the solar electric propulsion system technology program (SEPST 3) are reported and certain propulsion system-spacecraft interaction problems are discussed. The basic solar electric propulsion system concept and elements are reviewed.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::27342c5f4193c6a05b85195c79b5b681
https://doi.org/10.2514/6.1970-1153
https://doi.org/10.2514/6.1970-1153
Publikováno v:
9th Aerospace Sciences Meeting.
Oxide hollow cathode ion thruster power conditioner, evaluating electrical efficiency, weight, reliability integration and testing
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::606c14d768f2bffd5ffacdf87d036623
https://doi.org/10.2514/6.1971-159
https://doi.org/10.2514/6.1971-159