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Outer planet entry heating and thermal protection

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Raymond Viskanta
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American Institute of Aeronautics and Astronautics, Jan 1, 1979 - Technology & Engineering - 404 pages

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Contents

Effects of Atmospheric Structure on Radiative Heating
3
Radiative Flux Penetration through a Blown Shock Layer
22
Approximate In viscid Radiating Flowfieid Analysis
42
Copyright

15 other sections not shown

Common terms and phrases

ablation ablation layer absorption coefficient AIAA AIAA Journal AIAA Paper altitude analysis angle of attack atomic ballistic coefficient blockage blunted boundary layer bow shock calculations carbon carbon-phenolic chemical chemical equilibrium computed cone configuration convective heating correlation corrugation energy enthalpy entry conditions environment equations equilibrium experimental flow flowfield freestream graphite Heat Transfer heat-shield recession heat-transfer helium hydrogen hyperboloid inertial entry angle inviscid Jovian entry Jupiter entry km/sec laminar line widths mass loss material model atmospheres NASA nominal nondimensional nonequilibrium number density obtained Outer Planet Entry parameters phenolic Planet Entry Probes precursor heating precursor region predicted present pressure Progress in Astronautics radiation radiative and convective radiative flux radiative heating rates Reynolds number shield shock Shock Tube shock-layer shown in Fig solution Spacecraft species spectral sphere-cone stagnation point stagnation-point Table temperature thermal thermochemical thermodynamic Thermophysics tion trajectory turbulent uncertainty velocity wall

Bibliographic information

QR code for Outer planet entry heating and thermal protection
TitleOuter planet entry heating and thermal protection
Volume 64 of Progress in astronautics and aeronautics
Outer planet entry heating and thermal protection
EditorRaymond Viskanta
ContributorRaymond Viskanta
Editionillustrated
PublisherAmerican Institute of Aeronautics and Astronautics, 1979
Original fromthe University of Michigan
Digitized13 Dec 2007
ISBN0915928299, 9780915928293
Length404 pages
Subjects › 

Astronautics
Jupiter probes
Space flight
Space vehicles
Technology & Engineering / Aeronautics & Astronautics
  
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