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Thermal Design Principles of Spacecraft and Entry Bodies
- 1st Edition - December 2, 2012
- Editor: Jerry Bevans
- Language: English
- eBook ISBN:9 7 8 - 0 - 3 2 3 - 1 4 2 1 1 - 3
Progress in Astronautics and Aeronautics, Volume 21: Thermal Design Principles of Spacecraft and Entry Bodies is a collection of technical papers drawn mainly from the American… Read more
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Request a sales quoteProgress in Astronautics and Aeronautics, Volume 21: Thermal Design Principles of Spacecraft and Entry Bodies is a collection of technical papers drawn mainly from the American Institute of Aeronautics and Astronautics Third Thermophysics Specialist Conference, held in Los Angeles, California on June 24-26, 1968 This volume is divided into three parts. The first part covers some aspects of thermal processes and design, including thermal analysis, convection, radiation, ablation, and space rocket effects. The second part surveys the remote measurements of the thermophysical and thermal radiation properties and joint conductance, which are critical criteria for space thermal design. The third part focuses on the space environmental effects on thermal coatings. This part deals first with the theory of radiative degradation, followed by a presentation of the laboratory measurements. This part also looks into the results of several flight experiments. This book will be of great value to thermophysicists, space engineers, and designers who are working in the space science fields.
The Thermophysics Committee, 1967 and 1968
Preface
Editorial Committee for Volume 21
I. Thermal Processes and Thermal Design
I.1 Thermal Analysis
Higher-Order Approximations for Lumped System Analysis of Evacuated Enclosures
Optical Measurements of the Radiation Configuration Factor
Optical Shape Factor Data Processing through Computer Graphics
An Experimental Technique for Measuring Local Solar Irradiation with a Model Spacecraft
An Approximate Analytic Solution of the Steady-State Thermal Design Problem of Space Radiators
I.2 Entry Heating: Convection, Radiation, and Ablation
Radiative Transport in Inviscid Nonadiabatic Stagnation-Region Shock Layers
Radiation Transfer through High-Temperature Shock Layers
Remote Sensing of Rarefied Gas Flows through a Fluorescence Technique
Thermodynamic Performance of Carbon in Hyperthermal Environments
A Rapid Technique for Estimating Ablative Heat Shield Weights from Plasma Jet Test Data
Surface Oxidation with Streamwise Variation of Wall Reactivity
Hypersonic, Diffusion-Controlled Oxidation of Tungsten
I.3 Rocket Exhaust Effects
Spectral Radiance of Model Rocket Exhaust Plumes at High Altitudes
Effects of the LM Descent Engine Exhaust on Lunar Surface Temperatures
I.4 Lunar and Planetary Vehicles Design
A Study of the Thermal Kill of Viable Organisms during Mars Atmospheric Entry
Prediction of the Martian Thermal Environment
Thermal Control Aspects of a Stationary Martian Surface Laboratory
Thermal Testing under Simulated Martian Environment
LM Passive Thermal Design and Test
II. Thermophysical Properties for Design
II.1 Remote Measurements
Determination of Optical and Physical Properties of Artificial Satellites by Passive Ground-Based Photometry
Predicting Lunar Temperatures
Lunar Surface Thermal Characteristics during Eclipse from Surveyors III, V and after Sunset from Surveyor V
II.2 Thermal Radiation Properties
Emission, Total Internal Reflection, and Tunneling of Thermal Radiation in Metals
Measurements of Thermal Radiation of Solids at Liquid-Helium Temperatures
A Technique for the Measurement of Spectral Reflectances at Low Temperatures in the Infrared and Far Infrared
Development of Phase-Change Coatings
II.3 Joint Conductance
Simultaneous Radiation and Conduction between Rough Surfaces
Thermal Conductance of Two-Dimensional Constrictions
An Exact Solution for Thermal Conduction through a Two-Dimensional Eccentric Constriction
Effects of Transient Pressure Environments on Heat Transfer in One-Dimensional Composite Slabs with Contact Resistance
III. Space Environmental Effects Upon Thermal Coatings
III.1 Theory of Radiative Degradation
An Analytical Study of Solar Degradation Model for Thermal Control Materials and Some Ramifications for Accelerated Solar Radiation Testing
III.2 Laboratory Measurements
Effects of Extreme Ultraviolet on the Optical Properties of Thermal Control Coatings
Electron-Ultraviolet Radiation Effects on Thermal Control Coatings
Effects of Combined Electron-Ultraviolet Irradiation on Thermal Control Coatings in Vacuo at 77°K
The Development of S-13G-Type Thermal-Control Coatings
III.3 Flight Experiments
Results from the Thermal Control Coatings Experiment on OSO-III
Environmental Studies of Thermal Control Coatings for Lunar Orbiter
Thermal Control Experiments on the Lunar Orbiter Spacecraft
Contributors to Volume 21
- No. of pages: 876
- Language: English
- Edition: 1
- Published: December 2, 2012
- Imprint: Academic Press
- eBook ISBN: 9780323142113