Fundamentals of spacecraft thermal design Edited by John W. Lucas.

Fundamentals of spacecraft thermal design

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Bibliographic Details
Corporate Authors: AIAA Aerospace Sciences Meeting, AIAA Thermophysics Conference
Other Authors: Lucas, John W., 1923- (Editor)
Format: Electronic Conference Proceeding eBook
Language:English
Published: Cambridge, Mass., MIT Press [1972]
Series:Progress in astronautics and aeronautics ; v. 29.
Subjects:
Space vehicles > Thermodynamics > Congresses.
Online Access: Full text (Wentworth users only)
Local Note:ProQuest Ebook Central
Table of Contents:
  • 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 Protonsâ€?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

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