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Fundamentals of spacecraft thermal design
| Clasificación: | Libro Electrónico |
|---|---|
| Autores Corporativos: | , |
| Otros Autores: | |
| Formato: | Electrónico Congresos, conferencias eBook |
| Idioma: | Inglés |
| Publicado: |
Cambridge, Mass.,
MIT Press
[1972]
|
| Colección: | Progress in astronautics and aeronautics ;
v. 29. |
| Temas: | |
| Acceso en línea: | Texto completo |
Tabla de Contenidos:
- Cover
- Title
- Copyright
- Contents
- Preface
- Editorial Committee for Volume 29
- I. Surface Radiation Properties
- I.1 Synthesis and Measurement
- Space Radiation Environmental Effects on Reactively Encapsulated Zinc Orthotitanates and Their Paints
- Coloration of MgO Single Crystals by Low Energy Protons�A Function of Selected Defects
- Reflectance Measurements of Dielectric Coatings on a Conductor Substrate
- Bidirectional Reflectance of a Randomly Rough Surface
- Bidirectional Reflectance Characteristics of Integrating Sphere Coatings
- Particulate Radiation Effects on the Solar Absorptance of Thermal Control SurfacesLong-Duration Exposure of Spacecraft Thermal Coatings to Simulated Near-Earth Orbital Conditions
- I.2 Contamination Effects
- Sensitivity of Thermal Surface Solar Absorptance to Particulate Contamination
- Measurement and Application of Contaminant Optical Constants
- Restoration of Degraded Spacecraft Surfaces Using Reactive Gas Plasmas
- I.3 Space Flight Effects
- Report on the Flight Performance of the Z-93 White Paint Used in the SERT II Thermal Control System
- Radiation Degradation Analysis of Surveyor III MaterialStudy of Thermal Control Surfaces Returned from Surveyor III
- II. Thermal Analysis
- Directional Property Effects on Radiant Heat Transfer and Equilibrium Temperature
- Radiant Heat Transfer between Nongray Surfaces
- Thermal Contact Conductance of Turned Surfaces
- Thermal Conductance of a Row of Cylinders Contacting Two Planes
- Re-entry Thermal Analysis of Variable Thickness Spherical Vehicles
- Coupling of Shape Change, Heating Distribution and Internal Conduction for Ablating Bodies
- Temperature Uncertainties Associated with Spacecraft Thermal AnalysesSpacecraft Thermal Design Verification through Modeling
- III. Heat Pipes
- Effects of Friction on the Sonic Velocity Limit in Sodium Heat Pipes
- Possible Application of Electro-Osmotic Flow Pumping in Heat Pipes
- Experimental Performance of Grooved Heat Pipes at Moderate Temperatures
- Operating Characteristics and Long Life Capabilities of Organic Fluid Heat Pipes
- Design and Performance of Noncondensible Gas Controlled Heat Pipes
- Feedback Controlled Variable Conductance Heat Pipes
- Design, Fabrication, and Testing of a Variable Conductance Heat Pipe for Equipment Thermal ControlA Variable Conductance Heat-Pipe Flight Experiment
- IV. Thermal Design
- Apollo Telescope Mount/Thermal Systems Unit: Correlation of Predicted Data and Test Results
- Radiative, Ablative, and Active Cooling Thermal Protection Studies for the Leading Edge of a Fixed-Straight Wing Space Shuttle
- Space Station Environmental Thermal Control System Definition
- Index to Contributors to Volume 29
- A
- B
- C
- D
- E
- F
- G
- H
- J
- K
- L