Zobrazeno 1 - 10
of 15
pro vyhledávání: '"J. H. Molitor"'
Publikováno v:
Journal of Spacecraft and Rockets. 6:1285-1290
The potential performance advantages of solar electric propulsion have led to a study of the over-all spacecraft systems implications of such propulsion devices. The results of this study, including spacecraft design and trajectory analysis (using th
Publikováno v:
Journal of Spacecraft and Rockets. 3:554-560
Because of the long-time operation (^10,000 hr) required for most space missions, electric propulsion system reliability is a major problem. Since establishment of highcomponent reliability at high confidence levels is both time-consuming and costly,
Autor:
D. G. Elliott, J. H. Molitor
Publikováno v:
IRE Transactions on Space Electronics and Telemetry. :183-187
This paper discusses the requirements that must be met by electric thrust devices in order to be used with interplanetary spacecraft. Two missions, a Mars orbiter and a Jupiter capture, chosen as representative of the time periods following 1965 and
Autor:
J. H. Molitor, M. H. Kaplan
Publikováno v:
Journal of Spacecraft and Rockets. 2:712-718
Nomenclature A = earth's oblateness coefficient Ad = satellite drag area Ac = satellite area exposed to solar radiation c = speed of light in a vacuum Cd = satellite coefficient of atmospheric drag iQ = initial inclination of the satellite orbit K2 =
Publikováno v:
Journal of Spacecraft and Rockets. 4:603-609
Autor:
J. H. Molitor, K. J. Russell
Publikováno v:
Journal of Spacecraft and Rockets. 8:506-513
Mars and Venus orbiter spacecraft electric propulsion system, discussing Hg electron bombardment ion engine
Publikováno v:
Journal of Spacecraft and Rockets. 5:933-940
Solar electric propulsion for space missions, evaluating modularized ion propulsion systems to determine effect of electric isolation on system reliability, weight, etc
Autor:
R. N. Olson, J. H. Molitor
Publikováno v:
Journal of Spacecraft and Rockets. 5:1312-1318
Electric propulsion ion engine systems using solar power source for Mars and Jupiter exploratory unmanned spacecraft is adaptable to existing launch vehicles
Publikováno v:
Journal of Spacecraft and Rockets. 7:164-169
Electric propulsion design, considering effects of weight, impedance matching, beam voltage regulation and operating point variations in formulating system mass and reliability
Autor:
J. H. Molitor
Publikováno v:
12th International Electric Propulsion Conference.