Zobrazeno 1 - 10
of 36
pro vyhledávání: '"Franklin Chang-Diaz"'
Autor:
Ronald J. Litchford, Robert W. Moses, Mark Carter, Dennis M. Bushnell, Sang Choi, Franklin Chang-Diaz, David R. Komar
Publikováno v:
2018 AIAA SPACE and Astronautics Forum and Exposition.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2a7782005ded7c99cc6024b7837aa887
https://doi.org/10.2514/6.2018-5360
https://doi.org/10.2514/6.2018-5360
Autor:
Jared P. Squire, Greg McCaskill, Mark Carter, Lawrence Dean, Matthew Giambusso, Joseph Farrias, Aidan Corrigan, Tiffany Yao, Franklin Chang-Diaz
Publikováno v:
2018 Joint Propulsion Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8b8c1da764d2f0cd1fe1c70aa13160a2
https://doi.org/10.2514/6.2018-4504
https://doi.org/10.2514/6.2018-4504
Autor:
Franklin Chang Díaz, Erik Seedhouse
As advanced in-space propulsion moves from science fiction to reality, the Variable Specific Impulse Magnetoplasma Rocket, or VASIMR® engine, is a leading contender for making'Mars in a month'a possibility. A paradigm shift in space transpor
Publikováno v:
Journal of Materials Science. 47:4211-4235
The current review uses the material requirements of a new space propulsion device, the Variable Specific Impulse Magnetoplasma Rocket (VASIMR®) as a basis for presenting the temperature dependent properties of a range of dielectric ceramics, but da
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::92e0f0413f3b12dfce15c4ea65e609d3
https://doi.org/10.1007/s10853-011-6140-1
https://doi.org/10.1007/s10853-011-6140-1
Autor:
Edgar A. Bering, Benjamin W. Longmier, Jared P. Squire, Leonard D. Cassady, Franklin Chang-Diaz, Tim W. Glover, Maxwell G. Ballenger, Chris S. Olsen, Mark Carter, A. V. Ilin, Greg McCaskill
Publikováno v:
Journal of Propulsion and Power. 27:915-920
H IGH-POWER electric propulsion thrusters can reduce propellant mass for heavy-payload orbit-raising missions and cargo missions to the moon and near-Earth asteroids, and they can reduce the trip time of robotic and piloted planetary missions [1–4]
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::495c35329b6c259006e74250518cdf3a
https://doi.org/10.2514/1.b34085
https://doi.org/10.2514/1.b34085
Autor:
Edgar A. Bering, Franklin Chang-Diaz, T. W. Glover, Greg McCaskill, Roger D. Bengtson, Michael Brukardt, V. T. Jacobson, Jared P. Squire, L. D. Cassady
Publikováno v:
Advances in Space Research. 42:192-205
Plasma physics has found an increasing range of practical industrial applications, including the development of electric spacecraft propulsion systems. One of these systems, the Variable Specific Impulse Magnetoplasma Rocket (VASIMR) engine, both app
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::26a04f73c516b8cb5cc004b5e94d84d3
https://doi.org/10.1016/j.asr.2007.09.034
https://doi.org/10.1016/j.asr.2007.09.034
Publikováno v:
Journal of Propulsion and Power. 22:637-644
An impact target plate was used to determine the momentum and heat flux quantities from a helicon plasma source. The plasma source is the first stage of the Variable Specific Impulse Magnetoplasma Rocket, which uses radio frequency waves to create an
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::89a16064ba5a7e80f63bc11918ef887b
https://doi.org/10.2514/1.1971
https://doi.org/10.2514/1.1971
Autor:
Franklin Chang-Diaz
Publikováno v:
Thin Solid Films. :449-453
The Variable Specific Impulse Magnetoplasma Rocket (VASIMR) is a high-power propulsion concept using radio waves to create and accelerate plasma in a magnetic nozzle. Important features are its high and variable exhaust velocity, which greatly enhanc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9632b89ed909ad0b89ae3bfaf4b76e63
https://doi.org/10.1016/j.tsf.2005.08.324
https://doi.org/10.1016/j.tsf.2005.08.324
Autor:
Franklin Chang-Diaz, Mark D. Carter, T. W. Glover, Greg McCaskill, Richard Goulding, Jared P. Squire, D. Scott Winter, F. Wally Baity, V. T. Jacobson
Publikováno v:
Thin Solid Films. :579-582
In the Advanced Space Propulsion Laboratory (ASPL) helicon experiment (VX-10) we have measured a plasma flux to input gas rate ratio near 100% for both helium and deuterium at power levels up to 10 kW. Recent results at Oak Ridge National Laboratory
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cea5834437d624d082f27b408485fec6
https://doi.org/10.1016/j.tsf.2005.08.061
https://doi.org/10.1016/j.tsf.2005.08.061
Autor:
Richard Goulding, Jared P. Squire, Franklin Chang-Diaz, E. F. Jaeger, Mark D. Carter, F.W. Baity, Y. Mori, D. O. Sparks, G.C. Barber, K. F. White
Publikováno v:
ResearcherID
The ability to obtain high plasma densities with high fractional ionization using readily available, low-cost components makes the helicon a candidate plasma source for many applications, including plasma rocket propulsion, fusion component testing,
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::60366499c0b5cd801181d010d70d4bab
https://doi.org/10.13182/fst03-a11963578
https://doi.org/10.13182/fst03-a11963578