Thermophysics and spacecraft thermal control : technical papers selected from the AIAA 11th Aerospace Sciences Meeting, January 1973, and the AIAA 8th Thermophysics Conference, July 1973, subsequently revised for this volume /

Detalles Bibliográficos
Clasificación:Libro Electrónico
Autores Corporativos: AIAA Aerospace Sciences Meeting, AIAA Thermophysics Conference
Otros Autores: Hering, Robert G.
Formato: Electrónico Congresos, conferencias eBook
Idioma:Inglés
Publicado: Cambridge, Mass. : MIT Press, [1974]
Colección:Progress in astronautics and aeronautics ; v. 35.
Temas:
Space vehicles > Thermodynamics > Congresses.
Véhicules spatiaux > Thermodynamique > Congrès.
Space vehicles > Thermodynamics
Space vehicles > Thermal properties Conference proceedings
Conference papers and proceedings
Acceso en línea:Texto completo
Tabla de Contenidos:
  • Cover
  • Title
  • Copyright
  • Table of Contents
  • Preface
  • Editorial Comittee For Volume 35
  • I Radiative Heat Transfer
  • Comparison of Three Techniques for Solving the Radiative Transport Equation
  • Spherical Harmonics Approximation for Radiative Transfer in Polluted Atmospheres
  • Approximate Configuration Factors for a Gray Nonisothermal Gas-Filled Conical Enclosure
  • Radiation Heat Transfer in Multilayer Insulation Having Perforated Shields
  • A Thick-Thin Approximation for Radiative Transfer
  • Thermal Modeling of a Plate with Coupled Heat-Transfer Modes II Surface Radiation Properties
  • Reflectance from Semi-Infinite Absorbing-Scattering Medium with Diffuse Incident Radiation
  • Effect of Boundary Conditions on the Radiative Reflectance of Dielectric Coatings
  • Surface Roughness Effects on Bidirectional Reflectance
  • Diffraction Effects Encountered in the Measurement of Bidirectional Reflectance from Square Pyramids
  • Infrared Properties of Reusable Surface Insulations
  • A High-Speed (Subsecond) System for Accurate Thermophysical Measurements at High Temperatures Optical Properties of Cryodeposits on Low Scatter Mirrors
  • Optical Stability of Coatings Exposed to Four Years Space Environment on OSO-111
  • III Conduction and Joint Conductance
  • A General Expression for Predicting Conduction Shape Factors
  • Modeling the Effect of Air and Oil upon the Thermal Resistance of a Sphere-Flat Contact
  • Thermal Contact Conductance of Porous Metallic Materials in a Vacuum Environment
  • Thermal Conductance of Gasket Materials for Spacecraft Joints IV Heat Pipes
  • Gas Occlusions in Arterial Heat Pipes
  • A Probabilistic Approach to the Design of Heat Pipes
  • Development of a High Capacity Cryogenic Heat Pipe
  • Advanced Thermal Control Flight Experiment
  • Heat-Pipe System for Space Shuttle Traveling Wave Tube Amplifier
  • Orbiting Astronomical Observatory Heat Pipe Flight Performance Data
  • V Thermal Control of Spacecraft Systems
  • Analytical Modeling of Spacecraft with Heat Pipes and Louvers
  • Thermal Control of the Large Space Telescope Thermal Design of a Saturn/Uranus Atmospheric Entry Probe
  • Thermal Control of the Apollo 17 Lunar Traverse Gravimeter
  • Temperature Control of the Mariner-Class Spacecraft: A Seven-Mission Summary
  • Index of Contributors

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