scholarly journals Conceptual design of the National Ignition Facility

1995 ◽  
Author(s):  
Jeffrey A. Paisner ◽  
John D. Boyes ◽  
Steven A. Kumpan ◽  
W. Howard Lowdermilk ◽  
Michael S. Sorem
Keyword(s):  
Conceptual Design ◽  
National Ignition Facility

scholarly journals Conceptual Design of Low Activation Target Chamber and Components for the National Ignition Facility

1996 ◽  
Vol 30 (3P2A) ◽  
pp. 448-451 ◽  
Author(s):  
H.H. Streckert ◽  
K.R. Schultz ◽  
G.T. Sager ◽  
R.D. Kantncr
Keyword(s):  
Conceptual Design ◽  
Target Chamber ◽  
National Ignition Facility

The conceptual design of 1-ps time resolution neutron detector for fusion reaction history measurement at OMEGA and the National Ignition Facility

2020 ◽  
Vol 91 (6) ◽  
pp. 063304
Author(s):  
Yasunobu Arikawa ◽  
Masato Ota ◽  
Makoto Nakajima ◽  
Tomoki Shimizu ◽  
Sadashi Segawa ◽  
...  
Keyword(s):  
Conceptual Design ◽  
Time Resolution ◽  
Neutron Detector ◽  
Fusion Reaction ◽  
National Ignition Facility

Efficient Time-Independent Method for Conceptual Design Optimization of the National Ignition Facility Primary Shield

1995 ◽  
Vol 27 (4) ◽  
pp. 417-451 ◽  
Author(s):  
Ehud Greenspan ◽  
Cynthia E. Annese ◽  
Warren F. Miller ◽  
Edward F. Watkins ◽  
Michael L. Tobin ◽  
...  
Keyword(s):  
Design Optimization ◽  
Conceptual Design ◽  
Independent Method ◽  
National Ignition Facility

scholarly journals Conceptual design of the gamma-to-electron magnetic spectrometer for the National Ignition Facility

2014 ◽  
Vol 85 (11) ◽  
pp. 11E122 ◽  
Author(s):  
Y. Kim ◽  
H. W. Herrmann ◽  
H. J. Jorgenson ◽  
D. B. Barlow ◽  
C. S. Young ◽  
...  
Keyword(s):  
Conceptual Design ◽  
Magnetic Spectrometer ◽  
National Ignition Facility ◽  
Electron Magnetic Spectrometer

Innovative Conceptual Design

2001 ◽  
Author(s):  
Ehud Kroll ◽  
Sridhar S. Condoor ◽  
David G. Jansson
Keyword(s):  
Conceptual Design

Mass distribution of hydrodynamic jets produced on the national ignition facility

2006 ◽  
Vol 133 ◽  
pp. 107-110 ◽  
Author(s):  
B. E. Blue ◽  
S. V. Weber ◽  
D. T. Woods ◽  
M. J. Bono ◽  
S. N. Dixit ◽  
...  
Keyword(s):  
Mass Distribution ◽  
National Ignition Facility

ANALYSIS OF COMPETING VARIANTS OF AIR CONDITIONING SYSTEMS WITHOUT AIR EXTRACTION FROM ENGINES AT THE STAGE OF PASSENGER AIRCRAFT ONBOARD SYSTEMS CONCEPTUAL DESIGN

2019 ◽  
Vol 6 (3) ◽  
pp. 80-85
Author(s):  
Denis Igorevich Smagin ◽  
Konstantin Igorevich Starostin ◽  
Roman Sergeevich Savelyev ◽  
Anatoly Anatolyevich Satin ◽  
Anastasiya Romanovna Neveshkina ◽  
...  
Keyword(s):  
Conceptual Design ◽  
Air Conditioning ◽  
Research University ◽  
Cooling System ◽  
Fuel Efficiency ◽  
Air Cooling ◽  
Moscow Aviation Institute ◽  
Air Conditioning System ◽  
Low Efficiency ◽  
Air Conditioning Systems

One of the ways to achieve safety and comfort is to improve on-board air conditioning systems.The use of air cooling machine determines the air pressure high level at the point of selection from the aircraft engine compressor. Because of the aircraft operation in different modes and especially in the modes of small gas engines, deliberately high stages of selection have to be used for ensuring proper operation of the refrigeration machine in the modes of the aircraft small gas engines. Into force of this, most modes of aircraft operation have to throttle the pressure of the selected stage of selection, which, together with the low efficiency of the air cycle cooling system, makes the currently used air conditioning systems energy inefficient.A key feature of the architecture without air extraction from the main engines compressors is the use of electric drive compressors as a source of compressed air.A comparative analysis of competing variants of on-board air conditioning system without air extraction from engines for longrange aircraft projects was performed at the Moscow Aviation Institute (National Research University).The article deals with the main approaches to the decision-making process on the appearance of a promising aircraft on-board air conditioning system at the stage of its conceptual design and formulated the basic requirements for the structure of a complex criterion at different life cycle stages.The level of technical and technological risk, together with a larger installation weight, will require significant costs for development, testing, debugging and subsequent implementation, but at the same time on-board air conditioning system scheme without air extraction from the engines will achieve a significant increase in fuel efficiency at the level of the entire aircraft.

Conceptual Design of Geophysical Microsatellite

2014 ◽  
Vol 10 (6) ◽  
pp. 5-15
Author(s):  
S.A. Matviyenko ◽  
Keyword(s):  
Conceptual Design
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