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Astrophysics / Plasma / Atmospheric entry / Electron / Speed of sound / Temperature / Shock wave / Physics / Chemistry / Aerodynamics


The Spacecraft Communications Blackout Problem Encountered during Passage or Entry of Planetary Atmospheres
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Document Date: 2002-08-22 19:34:50


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City

Madrid / Pasadena / /

Company

Predict Electron Density Aero / IBM / Jet Propulsion Laboratory / Langley Aero / Planetary Atmospheres D. D. / vF / /

Country

United States / Spain / /

Facility

Jet Propulsion Laboratory / California Institute of Technology / /

IndustryTerm

communications blackout / communications blackout condition / chemical equilibrium / free energy / aero-thermodynamic tools / carrier visibility / consecutive normal-shock solutions / communications antenna / chemical species / obsolete input/output devices / chemical equilibrium properties / plasma gas / chemical elements / specific chemical reaction / energy / energy contribution / deep-space communications / partial molal free energy / chemical description / electromagnetic energy / neutral gas mixture / chemical composition / normal-shock solution / gas constant / gas equation / entry vehicle communications / normal shock solution / energy equations / ight applications / chemical reaction potential energy / quiescent gas / /

MusicGroup

X / Apollo / /

OperatingSystem

Sun Solaris / /

Organization

California Institute of Technology / National Aeronautics and Space Administration / Mars Pathfinder mission / Apollo mission / /

Person

BOW SHOCK / Dwain Spencer / /

Position

HB / early Mars atmosphere model / RT / ln RT / ln dNi RT / /

Product

Horton / Apollo / Gemini / /

ProgrammingLanguage

FORTRAN II / FORTRAN 77 / C++ / /

ProvinceOrState

California / /

Technology

ATM / heat transfer / space communications / operating system / thermodynamics / Deep Space Network / aero / recombination / /

SocialTag