Zobrazeno 1 - 10
of 10
pro vyhledávání: '"B. G. Herron"'
Autor:
G. A. Work, B. G. Herron
Publikováno v:
Journal of Spacecraft and Rockets. 3:315-320
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::45551ac7f7421f6bb78a8d1fc6a66d8a
https://doi.org/10.2514/3.28446
https://doi.org/10.2514/3.28446
Publikováno v:
12th International Electric Propulsion Conference.
Electric propulsion has been shown to offer major advantages over the techniques currently employed for the control of earth satellites. For a user to realize these advantages, however, requires the availability of a proven, operationally flight-read
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4f38936897d7eb9a88c1570baca378ba
https://doi.org/10.2514/6.1976-1058
https://doi.org/10.2514/6.1976-1058
Autor:
Harry A. Owen, B. G. Herron, L. L. Ogborn, R.D. Middlebrook, Y. Yu, J. G. Ferrante, Gene W. Wester
Publikováno v:
1975 IEEE Power Electronics Specialists Conference.
The rap session provided an informal forum for dissemination of information on the state of the art in modeling and simulation of power processing systems. Merits of time domain and frequency domain approaches were debated and the use of these techni
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d1ac1dd013871b0cd70bd68398420959
https://doi.org/10.1109/pesc.1975.7085604
https://doi.org/10.1109/pesc.1975.7085604
Publikováno v:
13th International Electric Propulsion Conference.
An Engineering Model (EM) 8 cm Ion Thruster Propulsion Subsystem was developed for operation at a thrust level 5 mN (1.1 mlb) at a specific impulse 1 sub sp = 2667 sec with a total system input power P sub in = 165 W. The system dry mass is 15 kg wit
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8e4407799913df00bba95a002ac79b4b
https://doi.org/10.2514/6.1978-646
https://doi.org/10.2514/6.1978-646
Autor:
B. G. Herron
Publikováno v:
12th International Electric Propulsion Conference.
The 30-cm Hg electron-bombardment ion thruster presently under development has reached engineering model status and is generally accepted as the prime propulsion thruster module to be used on the earliest solar electric propulsion missions. This pape
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::48950cf62e6372269c839cc9c78768bb
https://doi.org/10.2514/6.1976-991
https://doi.org/10.2514/6.1976-991
Publikováno v:
7th Communications Satellite Systems Conference.
Electric propulsion systems derive their low overall mass, relative to chemical propulsion systems, from an optimized mix of independently controlled power and mass flow rate. A significant reduction in mass can be secured by substituting electric pr
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7fb2526cf9099878ceca1ba17da6bebc
https://doi.org/10.2514/6.1978-537
https://doi.org/10.2514/6.1978-537
Publikováno v:
10th Electric Propulsion Conference.
The development of a high performance ion propulsion system composed of an ion thruster and its associated power processing equipment, dictates the establishment of a mutually compatible set of electrical characteristics. A 30-cm thruster power proce
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::75fcda96035e8cce5f1f52dbb1d1cc9d
https://doi.org/10.2514/6.1973-1104
https://doi.org/10.2514/6.1973-1104
Autor:
S. Kami, B. G. Herron
Publikováno v:
8th Electric Propulsion Conference.
Thrust vector measuring device using floating suspension system for ion engines, detecting vertical tilt and horizontal drifts of floating platform
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a9d78f614d15cc907fcdfc47064b9fae
https://doi.org/10.2514/6.1970-1104
https://doi.org/10.2514/6.1970-1104
Publikováno v:
9th Electric Propulsion Conference.
The 30 cm thruster/power conditioning and control system discussed represents a significant milestone in the evolution of prime ion propulsion systems. The effort described covers three distinct electronic hardware implementation, integration and tes
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4ee31a496f64826c4ca7e79c6be9f010
https://doi.org/10.2514/6.1972-509
https://doi.org/10.2514/6.1972-509
Autor:
B. G. Herron, R. W. Opjorden
Publikováno v:
8th Electric Propulsion Conference.
High voltage solar array with integral power conditioning, discussing weight factors, panel design and layout, mechanization, performance prediction, etc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::58c59c00a23a0d4766ce20c3385d3de1
https://doi.org/10.2514/6.1970-1158
https://doi.org/10.2514/6.1970-1158