Zobrazeno 1 - 10
of 25
pro vyhledávání: '"Greg McCaskill"'
Autor:
Franklin R. Chang Díaz, Jared P. Squire, Aidan Corrigan, Joseph Farrias, Mark Carter, Lawrence Dean, Matthew Giambusso, Greg McCaskill, Tiffany Yao
Publikováno v:
AIAA Propulsion and Energy 2019 Forum.
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.
Autor:
Matthew Giambusso, Jared P. Squire, Lawrence Dean, Greg McCaskill, Mark Carter, Aidan Corrigan, Joseph Farrias, Franklin R. Chang Díaz, Tiffany Yao
Publikováno v:
2018 Joint Propulsion Conference.
Autor:
Matthew Giambusso, Franklin R. Chang Díaz, Mark Carter, Jared P. Squire, Edgar A. Bering, Greg McCaskill
Publikováno v:
2018 Joint Propulsion Conference.
Autor:
Franklin R. Chang Díaz, Mark Carter, Lawrence Dean, Matthew Giambusso, Jared P. Squire, Greg McCaskill, Tiffany Yao, Joseph Farrias, Aidan Corrigan
Publikováno v:
2018 Joint Propulsion Conference.
Autor:
Juan Del Valle, Jose Castro, Lawrence Dean, Franklin R. Chang Díaz, Aidan Corrigan, Greg McCaskill, Matthew Giambusso, Mark Carter, Jared P. Squire, Tim W. Glover
Publikováno v:
53rd AIAA/SAE/ASEE Joint Propulsion Conference.
Autor:
Benjamin W. Longmier, Jared P. Squire, Maxwell G. Ballenger, Edgar A. Bering, Mark D. Carter, Franklin R. Chang Díaz, Andrew V. Ilin, Greg McCaskill, Tim W. Glover, Chris S. Olsen, Leonard D. Cassady
Publikováno v:
Journal of Propulsion and Power. 30:123-132
Testing of the Variable Specific Impulse Magnetoplasma Rocket VX-200 engine was performed over a wide throttle range in a 150 m3 vacuum chamber with sufficient pumping to permit exhaust plume measurements at argon background pressures less than 1×10
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]
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
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