Thermophysics and temperature control of spacecraft and entry vehicles /
Thermophysics and Temperature Control of Spacecraft and Entry Vehicles.
Clasificación: | Libro Electrónico |
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Autores Corporativos: | , |
Otros Autores: | |
Formato: | Electrónico Congresos, conferencias eBook |
Idioma: | Inglés |
Publicado: |
New York :
Academic Press,
1966.
|
Colección: | Progress in astronautics and aeronautics ;
v. 18. |
Temas: | |
Acceso en línea: | Texto completo |
Tabla de Contenidos:
- Cover
- Title
- Copyright
- The Thermophysics Committee 1965
- The Thermophysics Committee 1966
- Preface
- Contents
- I. Thermal Radiation Properties of Solids
- Far Infrared Reflectance of Spacecraft Coatings
- Low-Temperature Spectral Emittance Measurements
- Total Normal Emittance Measurements to 2200°C in Air
- Solar Absorptance and Thermal Emittance of Aluminum Coated with Surface Films of Evaporated Aluminum Oxide
- Low-Temperature Emittance Determinations
- Thermal Radiation Properties of Binary Mixtures
- Directionally Reflective Coating StudyApparatus for Spectral Bidirectional Reflectance Measurements During Ultraviolet Irradiation in Vacuum
- Total Hemispherical Thermal Emittance of Nickel as a Function of Oxide Thickness in the Temperature Range 400°-900°C
- Effect of Surface Roughness on Emittance of Nonmetals
- Radiant Heat Transfer from Nongray Surfaces with External Radiation
- II. Lunar and Planetary Thermal Environment
- Effect of Specular Ground Reflection on Radiation Leaving Top of a Planetary Atmosphere
- Effect of Surface Properties on Planetary AlbedoIrradiation above Atmosphere Due to Rayleigh Scattering and Diffuse Terrestrial Reflections
- Theory of Diffuse Spectral Reflectance of a Thick Layer of Absorbing and Scattering Particles
- Far-Infrared Studies of Silicate Minerals
- Directional Radiative Characteristics of Conical Cavities And Their Relation To Lunar Phenomena
- III. Effects of the Space Environment on Optical Properties of Thermal Control Surfaces
- Low-Energy Charged Particle Environment of the Earth
- Exploratory Trapped-Particle and Trapped-Particle-Plus-Ultraviolet Effects on the Optical Properties of Spacecraft Thermal Control CoatingsEffects of Simulated Solar-Wind Bombardment on Spacecraft Thermal Control Surfaces
- Effects of Low Energy Protons on Thermal Control Coatings
- Effects of Protons and Alpha Particles on Thermal Properties of Spacecraft and Solar Concentrator Coatings
- Mariner-Mars Absorptance Experiment
- Preliminary Results from the Ames Emissivity Experiment on OSO-II
- SNAP 10A Thermal Control Coatings
- IV. Physics of Vehicle and Missile EntryDetermination of Temperature Profile in Charred Phenolic Composites by Reconstruction of the Ablation Process
- Effects of Uncertainties in Thermophysical Properties on Ablation Efficiency
- Determination of Thermal Performance of Char under Heating Conditions Simulating Atmospheric Entry
- Ablation of Magnesia
- Thermal Diffusivity Measurements of Graphites and Chars Using a Pulsed Laser
- V. Thermal Modeling and Interface Conductance in Space
- Test on a Thermally Scaled Model Space Station in a Simulated Solar Environment