«ABLATIVELY» 관련 영어 책
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1
Properties of
Ablatively Accelerated Targets
Targets are ablatively accelerated to high velocity (> 10 to the 7th power cm/s) with good hydrodynamic efficiency (about 20%) using low-irradiance (10 to the 13th power - 10 to the 14th power) long (3 - 4 ns) Nd-laser pulses.
B. H. Ripin, S. E. Bodner, S. H. Gold, 1980
2
Beam Nonuniformity Effects on Laser
Ablatively Accelerated ...
A laser doppler shift technique gives the velocity profiles of ablatively accelerated targets.
S. P. Obenschain, R. H. Lemberg, B. H. Ripin, 1980
3
Uniformity of Laser-Driven,
Ablatively Accelerated Targets
A double-target technique is used to measure the uniformity with which laser irradiated thin foil targets are ablatively accelerated.
S. P. Obenschain, B. H. Ripin, Naval Research Laboratory (U.S.), 1981
4
Preheat Studies on Laser
Ablatively-Accelerated Foils
The achievement of laser fusion requires the inward acceleration of pellet shells to very high velocity without excessive preheat of the pellet fuel.
E. A. McLean, Naval Research Laboratory (U.S.), S. H. Gold, 1980
5
Nuclear Fusion by Inertial Confinement: A Comprehensive Treatise
Emery, M. H., Dahlburg, J. P., and Gardner, J. H., The Rayleigh- Taylor instability
in ablatively accelerated targets with 1, 1/2, 1/4 (im laser light, Phys. Fluids, 31 (N
5), 1007, 1988. 76. Gamaly, E. G., Rozanov, V. It., Samarsky, A. A., Tishkin, V. F. ...
Guillermo Velarde, Yigal Ronen, Jose M. Martinez-Val, 1992
6
Experiments on the Dynamics and Hydrodynamic Instabilities ...
Experiments on pressure and velocity of accelerated foils were conducted using the double foil technique or actual laser foil experiments.
MISSION RESEARCH CORP ALEXANDRIA VA., 1983
7
The Rayleigh-Taylor Instability in
Ablatively Accelerated ...
The results of a series of detailed numerical simulations are presented for the Rayleigh-Taylor instability in laser ablatively accelerated targets for a fairly wide range of initial conditions.
Mark H. Emery, Jill P. Dahlburg, John H. Gardner, 1987
Experimental results on ablatively accelerated pellet implosions have been
encouraging, with respect to both implosion velocities and compression factors
achieved, but the uniformity of the implosion is not yet adequate for compression
to ...
Panel on the Physics of Plasmas and Fluids, Physics Survey Committee, Board on Physics and Astronomy, 1986
9
Laser-Plasma Interactions 4
Because the temperatures achieved with ablatively driven targets are much lower
than with exploding-pushers, and because the thicker shells absorb more
strongly, emission spectroscopy is much less easy with ablatively driven targets.
10
Proceedings of DAE-BRNS National Laser Symposium.
When the ablatively accelerated case was considered, variation of k from 9.71 x
I04-9.83x I04 m" 1 slightly decreases y from 5.836 x I08 - 5.791 x 10* sec'1. When
V3 is increased from 3 x 101 - 4.5 x lo'm/sec growth rate shows a sharp ...
Board of Research in Nuclear Sciences, Department of Atomic Energy, 2002
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Unlocking the secrets of star creation
Kane said the Eagle Nebula project not only provides insights into how pillar structures form in HII regions—and whether an ablatively confined ... «Phys.Org, 4월 15»
Launch your own satellite for US$8000
Each Common Propulsion Module is composed of four propellant tanks and a single throttleable, ablatively-cooled rocket engine. The rocket ... «Gizmag, 4월 12»
Falcon 1 launches with RazakSat for Malaysia's ATSB
This residual thrust was determined to have been the result of the replacement of the ablatively cooled Merlin-1A engine used on the previous ... «NASASpaceflight.com, 7월 09»
Why Mars is more important than cosmetics and why a failed launch …
Instead of cooling the combustion chamber ablatively, by letting the chamber burn away slowly from the inside, the Merlin cooled it ... «IEEE Spectrum, 5월 09»
SpaceX Determines Cause of Falcon 1 Launch Failure
The gap between engine cut off and staging was 1.5 seconds - which was fine for the ablatively cooled engine on Flight 2. But on Flight 3, with ... «Space Ref, 8월 08»
Collision between rocket stages doomed Falcon 1
"The Re-gen engine has a much longer thrust transient than the ablatively-cooled engine," Musk said. In the Merlin 1C's cooling system, ... «Spaceflight Now, 8월 08»
