Zobrazeno 1 - 10
of 38
pro vyhledávání: '"Francis M. Curran"'
Autor:
Francis M. Curran
Publikováno v:
Civil War History. 66:93-95
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0321b563112eb46777463cb3245b666e
https://doi.org/10.1353/cwh.2020.0013
https://doi.org/10.1353/cwh.2020.0013
Autor:
Francis M. Curran
Publikováno v:
West Virginia History: A Journal of Regional Studies. 13:99-101
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::083ef3d6a950283cbd5f1fecf1b3fc8e
https://doi.org/10.1353/wvh.2019.0005
https://doi.org/10.1353/wvh.2019.0005
Autor:
III, Francis M. Curran1 (AUTHOR)
Publikováno v:
Civil War History. Mar2020, Vol. 66 Issue 1, p93-95. 3p.
Publikováno v:
Acta Astronautica. 29:651-665
The NASA Lewis Research Center (LeRC) conducts and directs an electric propulsion research and technology program aimed at providing high-performance electric propulsion system options for a broad range of near and far-term missions. This evolutionar
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::96c05a5095eed4cec983e9e6f3d70790
https://doi.org/10.1016/0094-5765(93)90084-a
https://doi.org/10.1016/0094-5765(93)90084-a
Autor:
Michael J. Patterson, Francis M. Curran, Eric Pencil, John M. Sankovic, Vincent K. Rawlin, Thomas W. Haag, James S. Sovey
Publikováno v:
Acta Astronautica. 30:151-164
Near term flight applications of arcjet and ion thruster satellite station-keeping systems as well as development activities in Europe, Japan, and the United States are reviewed. At least two arcjet and three ion propulsion flights are scheduled duri
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d4479db070a8cf4ab2dcb42b27bc85b9
https://doi.org/10.1016/0094-5765(93)90107-8
https://doi.org/10.1016/0094-5765(93)90107-8
Autor:
Thomas W. Haag, Francis M. Curran
Publikováno v:
Journal of Spacecraft and Rockets. 29:444-452
An automated, cyclic life test was performed to demonstrate the reliability and endurance of a low power dc cycle arcjet thruster. Over 1000 hr and 500 on-off cycles were accumulated which would represent the requirements for about 15 years of on-orb
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cee9bd2890378a13008a252b2fb05a93
https://doi.org/10.2514/3.25484
https://doi.org/10.2514/3.25484
Publikováno v:
Space technology and applications international forum (STAIF - 97).
The combination of spacecraft electrical power and on-board propulsion can consume as much as three-fourths of the mass of a spacecraft depending upon the mission. With the current emphasis on reducing costs (including launch vehicle costs) and on re
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0f438e8ed73ce6cfa22f6db57b9953f2
https://doi.org/10.1063/1.52008
https://doi.org/10.1063/1.52008
Publikováno v:
16th International Communications Satellite Systems Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fb3d8b154ddb4769b3313550be043aed
https://doi.org/10.2514/6.1996-1142
https://doi.org/10.2514/6.1996-1142
Publikováno v:
34th Aerospace Sciences Meeting and Exhibit.
Onboard spacecraft power and propulsion are two of the essential utilities provided on a spacecraft. Together, these two subsystems can comprise one-half to over three-fourths of the launch mass of a spacecraft. What is not often realized is that the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fe2c847e4ef6e82eff1ead1f5d904858
https://doi.org/10.2514/6.1996-121
https://doi.org/10.2514/6.1996-121
Publikováno v:
31st Joint Propulsion Conference and Exhibit.
Solar electric propulsion (SEP) technology is currently being used for geostationary satellite station keeping to increase payload mass. Analyses show that advanced electric propulsion technologies can be used to obtain additional increases in payloa
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::d087ef81e5b64037ee86ad6631a2919f
https://doi.org/10.2514/6.1995-2513
https://doi.org/10.2514/6.1995-2513