Scientific and Technical Aerospace Reports Volume 38 July 28, 2000

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Page 1 and 2: Scientific and Technical Aerospace
Page 3 and 4: Introduction Scientific and Technic
Page 5 and 6: Subject Divisions Table of Contents
Page 7 and 8: ground equipment and systems. For a
Page 9 and 10: Subject Categories of the Division
Page 11 and 12: 48 Oceanography 139 Includes the ph
Page 13 and 14: 72 Atomic and Molecular Physics 191
Page 15 and 16: Document Availability Information T
Page 17: Avail: NASA Public Document Rooms.
Page 21 and 22: ALABAMA AUBURN UNIV. AT MONTGOMERY
Page 23 and 24: ��
Page 25 and 26: 20000061433 Pisa Univ., Dipartiment
Page 27 and 28: English; 34th; 34th Thermophysics C
Page 29 and 30: ciency of the generated derivative
Page 31 and 32: 20000063509 NASA Glenn Research Cen
Page 33 and 34: 05 AIRCRAFT DESIGN, TESTING AND PER
Page 35 and 36: A long tradition of aerodynamic des
Page 37 and 38: sonic and transonic cases will be p
Page 39 and 40: 20000061449 British Aerospace Publi
Page 41 and 42: 20000064593 NASA Langley Research C
Page 43 and 44: performance required for a proposed
Page 45 and 46: ment cost and create better product
Page 47 and 48: tion (NPSS), is focused on the inte
Page 49 and 50: surface measurement techniques used
Page 51 and 52: with emphasis on the search for lin
Page 53 and 54: 20000063520 NASA Kennedy Space Cent
Page 55 and 56: primary issues for it’s adaptatio
Page 57 and 58: Footage shows the night vertical ta
Page 59 and 60: 20000067665 NASA Kennedy Space Cent
Page 61 and 62: necessary for ignition modeling, or
Page 63 and 64: engine lifetime, and high power ope
Page 65 and 66: 24 COMPOSITE MATERIALS ��
Page 67 and 68: ments. For the screening of liner m
Page 69 and 70:
formation of a neutral, fluorescent
Page 71 and 72:
20000065655 Ames Lab., IA USA Funda
Page 73 and 74:
This is a second Triennial Conferen
Page 75 and 76:
of completely charged PSSNa solutio
Page 77 and 78:
20000064100 NASA Langley Research C
Page 79 and 80:
Spacecraft in low Earth orbit (LEO)
Page 81 and 82:
Pressure gradients, i.e. pressure h
Page 83 and 84:
agreed that the NO(sub x) levels co
Page 85 and 86:
tectural approach to extending the
Page 87 and 88:
20000064078 Physics and Electronics
Page 89 and 90:
20000064925 Institute for Human Fac
Page 91 and 92:
Page 93 and 94:
20000062455 National Inst. of Stand
Page 95 and 96:
Added Analysis (Risk Reduction); 6)
Page 97 and 98:
shipboard electrical power generati
Page 99 and 100:
20000067664 Jet Propulsion Lab., Ca
Page 101 and 102:
other, The theoretical framework go
Page 103 and 104:
figures compare the lift and pitchi
Page 105 and 106:
ment phase demonstrate desired feat
Page 107 and 108:
esolution mode with resolving power
Page 109 and 110:
to track 1% or 0.5% changes was hig
Page 111 and 112:
20000067643 NASA Marshall Space Fli
Page 113 and 114:
37 MECHANICAL ENGINEERING ��
Page 115 and 116:
solver based on overset grid techno
Page 117 and 118:
Page 119 and 120:
20000064621 Rensselaer Polytechnic
Page 121 and 122:
that for a specific example of a be
Page 123 and 124:
km x 1000 km). As with the nearly c
Page 125 and 126:
20000064527 Analytical Imaging and
Page 127 and 128:
20000064533 Austin State Univ., Dep
Page 129 and 130:
20000064539 California Univ., Inst.
Page 131 and 132:
Page 133 and 134:
in Yellowstone National Park. We ar
Page 135 and 136:
terns of community hysteresis based
Page 137 and 138:
Page 139 and 140:
tion model (DEM) fitting to the sca
Page 141 and 142:
The Carolina slate belt is a 10- to
Page 143 and 144:
20000063373 Los Alamos National Lab
Page 145 and 146:
20000064912 New Energy and Industri
Page 147 and 148:
and discusses the issues and resear
Page 149 and 150:
The objective of this study was to
Page 151 and 152:
distributions with engine test resu
Page 153 and 154:
7.6, while the 1926 events appear t
Page 155 and 156:
We investigate the compositional di
Page 157 and 158:
Flight Center, USA; Moore, T. E., N
Page 159 and 160:
This report presents the Applied Me
Page 161 and 162:
in Goa, India, by 3 - 4 days. Wind
Page 163 and 164:
51 LIFE SCIENCES (GENERAL) Includes
Page 165 and 166:
20000062717 Joint Inst. for Nuclear
Page 167 and 168:
Page 169 and 170:
during 50% (SD 4%) of the breathing
Page 171 and 172:
20000064711 Massachusetts Inst. of
Page 173 and 174:
The analysis of this smaller data s
Page 175 and 176:
vided a functional helmet mount. Th
Page 177 and 178:
61 COMPUTER PROGRAMMING AND SOFTWAR
Page 179 and 180:
The goal of multi-image classificat
Page 181 and 182:
20000063526 Defence Science and Tec
Page 183 and 184:
85 dB amplifier design evolved by o
Page 185 and 186:
20000064594 New Mexico Univ., Elect
Page 187 and 188:
20000064615 NASA Ames Research Cent
Page 189 and 190:
declarations with a pattern recogni
Page 191 and 192:
containing point where interpolatio
Page 193 and 194:
has his own responsibility, while t
Page 195 and 196:
the people, documents and projects
Page 197 and 198:
and experimental technology, many o
Page 199 and 200:
tems. In particular this applicatio
Page 201 and 202:
Over the past decade, high performa
Page 203 and 204:
expensive than a single analysis. I
Page 205 and 206:
20000064726 Carnegie-Mellon Univ.,
Page 207 and 208:
20000064099 Teledyne Brown Engineer
Page 209 and 210:
20000066597 Geophysical Observatory
Page 211 and 212:
20000065633 Institute TNO of Applie
Page 213 and 214:
important conclusion is that for su
Page 215 and 216:
est frame of the string. The modifi
Page 217 and 218:
isotopes. The method and program we
Page 219 and 220:
A detailed study is undertaken, usi
Page 221 and 222:
20000063497 Kaiser Electro-Optics,
Page 223 and 224:
delivers 60% of the x-ray flux from
Page 225 and 226:
76 SOLID-STATE PHYSICS ��
Page 227 and 228:
20000064660 Abdus Salam Internation
Page 229 and 230:
Page 231 and 232:
20000064703 Institute of Atomic Ene
Page 233 and 234:
The BRST approach is applied to the
Page 235 and 236:
20000067671 Hampton Univ., VA USA A
Page 237 and 238:
82 DOCUMENTATION AND INFORMATION SC
Page 239 and 240:
ecoming almost too cumbersome to be
Page 241 and 242:
physical world. These are the two p
Page 243 and 244:
with WFPC2 data. Tests of HSTphot
Page 245 and 246:
A brief description is given of the
Page 247 and 248:
20000064070 NASA Ames Research Cent
Page 249 and 250:
gas, show variations that have rema
Page 251 and 252:
egy, called Power In that would all
Page 253 and 254:
20000065631 NASA Kennedy Space Cent
Page 255 and 256:
20000064089 Smithsonian Astrophysic
Page 257 and 258:
A ABERRATION, 143, 198 ABRASION, 22
Page 259 and 260:
COMPRESSIBLE FLOW, 83 COMPRESSION L
Page 261 and 262:
FATIGUE (MATERIALS), 50, 93, 96 FAT
Page 263 and 264:
LASING, 90 LATE STARS, 224 LATITUDE
Page 265 and 266:
PATCH ANTENNAS, 74 PATHOLOGY, 98 PA
Page 267 and 268:
SPACE PLATFORMS, 38 SPACE PROBES, 2
Page 269 and 270:
WIND PROFILES, 137 WIND TUNNEL TEST
Page 271 and 272:
Brown, Andy, 38 Brown, April S., 20
Page 273 and 274:
Grosvenor, C. A., 70 Grosvenor, J.
Page 275 and 276:
Lu, Gui-Ying, 50 Lugg, Desmond J.,
Page 277 and 278:
Robertson, Tony, 39 Robinson, Jeffr
Page 279:
Warner, J. D., 63 Warren, James, 16
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Scientific and Technical Aerospace Reports Volume 38 July 28, 2000

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