Zobrazeno 1 - 8
of 8
pro vyhledávání: '"D. C. Byers"'
Autor:
R. L. Sackheim, D. C. Byers
Publikováno v:
Journal of Propulsion and Power. 14:669-675
In-space propulsion is required for multiple, critical, postlaunch functions for most space missions. The propulsion functions are broadly classi ed as insertion, on-orbit (including stationkeeping, repositioning, constellation management, etc.), a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9c6c2ae7fd749f29a76bff300c798645
https://doi.org/10.2514/2.5329
https://doi.org/10.2514/2.5329
Autor:
D. C. Byers
Publikováno v:
13th International Electric Propulsion Conference.
Information on the field and particle interfaces of electron bombardment ion thruster systems was summarized. Major areas discussed were the nonpropellant particles, neutral propellant, ion beam, low energy plasma, and fields. Spacecraft functions an
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::35ff9eba89156e82f0aae63416f4574e
https://doi.org/10.2514/6.1978-677
https://doi.org/10.2514/6.1978-677
Autor:
T. H. Silva, D. C. Byers
Publikováno v:
16th Joint Propulsion Conference.
The paper discusses a potential application of electric propulsion to perform orbit transfer of a large spacecraft structure to geosynchronous orbit (GEO) from LEO, utilizing a nuclear reactor space power source in the spacecraft on a shared basis. T
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7cedba1003fc8b76518323089060f671
https://doi.org/10.2514/6.1980-1223
https://doi.org/10.2514/6.1980-1223
Publikováno v:
Conference on Advanced Technology for Future Space Systems.
A general methodology is presented which allows prediction of the overall characteristics of thrust systems employing electron-bombardment ion thrusters. Elements of the thrust system are defined and their characteristics presented in a parametric fa
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::43d92d9498043c142370f4391d151411
https://doi.org/10.2514/6.1979-881
https://doi.org/10.2514/6.1979-881
Autor:
V. K. Rawlin, D. C. Byers
Publikováno v:
12th International Electric Propulsion Conference.
The results of an anlaysis of electron bombardment ion propulsion systems for use in the transportation and on-orbit operations of large space systems are presented. Using baseline technology from the ongoing primary propulsion program and other sour
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8e24b5b073dc669f22bd328fa05139d3
https://doi.org/10.2514/6.1976-1039
https://doi.org/10.2514/6.1976-1039
Autor:
D. C. Byers
Publikováno v:
14th International Electric Propulsion Conference.
The use of advanced electric propulsion systems is expected to provide cost and performance benefits for future energetic space missions. A methodology to predict the characteristics of advanced electric propulsion systems was developed and programme
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6b2224aa5f9abe05e8f1cd2ae04811eb
https://doi.org/10.2514/6.1979-2041
https://doi.org/10.2514/6.1979-2041
Publikováno v:
8th Electric Propulsion Conference.
SERT 2 spacecraft ion thrustor ground tests and flight operation, tabulating performance data
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::afddd8056c74b12744d49b7b51265485
https://doi.org/10.2514/6.1970-1125
https://doi.org/10.2514/6.1970-1125
Publikováno v:
6th Aerospace Sciences Meeting.
Mercury bombardment permanent magnet Kaufman thrustor using hollow cathode for SERT 2 mission, discussing performance characteristics and configurations
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0627d1bf83bf96ad163fd0ed7554644d
https://doi.org/10.2514/6.1968-88
https://doi.org/10.2514/6.1968-88