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151017s2000 xx o 000 0 eng d |
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|a EBLCP
|b eng
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|c EBLCP
|d OCLCO
|d OCLCQ
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|d OCLCQ
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|a 9781600863431
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|a 1600863434
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|a DEBBG
|b BV044094894
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|a (OCoLC)922978977
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|a TL900 ǂb A33 1982eb
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|a 629.44/1
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|a UAMI
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|a Bauer, Paul E.
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|a Entry Vehicle Heating and Thermal Protection Systems :
|b Space Shuttle, Solar Starprobe, Jupiter Galileo Probe.
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| 260 |
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|a Reston :
|b American Institute of Aeronautics and Astronautics,
|c 2000.
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| 300 |
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|a 1 online resource (588 pages)
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| 336 |
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|a text
|b txt
|2 rdacontent
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| 337 |
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|a computer
|b c
|2 rdamedia
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| 338 |
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|a online resource
|b cr
|2 rdacarrier
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| 490 |
1 |
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|a Progress in Astronautics and Aeronautics ;
|v v. 85
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| 588 |
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|a Print version record.
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|a ""Cover""; ""Title""; ""Copyright""; ""Table of Contents""; ""Preface""; ""Editorial Committee""; ""List of Series Volumes""; ""Chapter I. Space Shuttle Aeroheating""; ""Aerothermodynamic Entry Environment of the Space Shuttle Orbiter""; ""Approximate Method of Predicting Heating on the Windward Side of Space Shuttle Orbiter and Comparisons with Flight Data""; ""Viscous Shock-Layer Predictions for Hypersonic Laminar or Turbulent Flows in Chemical Equilibrium over the Windward Surface of a Shuttle-Like Vehicle""
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| 505 |
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|a ""Influence of Radiant Energy Exchange on the Determination of Convective Heat-Transfer Rates to Orbiter Leeside Surfaces during Entry""""Catalytic Efficiency of the Space Shuttle Heat Shield""; ""Catalytic Recombination/Space Shuttle Heating""; ""Viscous Shock-Layer Heating Analysis for the Shuttle Windward Symmetry Plane with Surface Finite Catalytic Recombination Rates""; ""Chapter II. Space Shuttle Thermal Protection""; ""Shuttle Orbiter Reusable Surface Insulation Thermal Performance""; ""Space Shuttle Orbiter Leading Edge Thermal Performance""
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| 505 |
8 |
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|a ""Comparison of Orbiter STS-2 Development Flight Instrumentation Data with Thermal Math Model Predictions""""Flight Measurements of Tile Gap Heating on the Space Shuttle""; ""Tile-Gap Flow in the Shuttle Orbiter Thermal Protection System""; ""Assessment of Alternate Thermal Protection Systemsfor the Space Shuttle Orbiter""; ""Initial Shuttle External Tank Aerothermal Flight Evaluation""; ""Chapter III. Solar Starprobe Heat Shielding""; ""STARPROBE Thermal Shield System Design Concepts""; ""Preliminary Design of the Thermal Protection System for Solar Probe""
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| 505 |
8 |
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|a ""Chapter IV. Jupiter Galileo Probe Entry Heating and Protection""""Galileo Probe Forebody Flowfield Predictions""; ""An Evaluation of Turbulence Models for Massively Blown Surfaces""; ""Trajectories of Solid Particles Spalled from a Carbonaceous Heat Shield""; ""Spallation of the Galileo Probe Heat Shield""; ""Response of Galileo Aft Cover Componentsto Laser Radiation""; ""Author Index for Volume 85""
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| 590 |
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|a ProQuest Ebook Central
|b Ebook Central Academic Complete
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| 650 |
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0 |
|a Space vehicles
|x Thermodynamics
|v Congresses.
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| 650 |
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0 |
|a Space vehicles
|x Atmospheric entry
|v Congresses.
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| 650 |
|
6 |
|a Véhicules spatiaux
|x Thermodynamique
|v Congrès.
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| 650 |
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6 |
|a Véhicules spatiaux
|x Entrée dans l'atmosphère
|v Congrès.
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| 650 |
|
7 |
|a Space vehicles
|x Atmospheric entry
|2 fast
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| 650 |
|
7 |
|a Space vehicles
|x Thermodynamics
|2 fast
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| 655 |
|
7 |
|a Conference papers and proceedings
|2 fast
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| 700 |
1 |
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|a Collicott, Howard E.
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| 758 |
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|i has work:
|a Entry vehicle heating and thermal protection systems (Text)
|1 https://id.oclc.org/worldcat/entity/E39PD33BgJwxxqwqJPkrqjw4pX
|4 https://id.oclc.org/worldcat/ontology/hasWork
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| 776 |
0 |
8 |
|i Print version:
|a Bauer, Paul E.
|t Entry Vehicle Heating and Thermal Protection Systems : Space Shuttle, Solar Starprobe, Jupiter Galileo Probe.
|d Reston : American Institute of Aeronautics and Astronautics, ©2000
|z 9780915928743
|
| 830 |
|
0 |
|a Progress in astronautics and aeronautics.
|
| 856 |
4 |
0 |
|u https://ebookcentral.uam.elogim.com/lib/uam-ebooks/detail.action?docID=3111587
|z Texto completo
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| 938 |
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|a ProQuest Ebook Central
|b EBLB
|n EBL3111587
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| 994 |
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|a 92
|b IZTAP
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