SAE AIR 1168/12 : 2011
SAE AIR 1168/12 : 2011
SPACECRAFT THERMAL BALANCE
SAE International
Specials
-
-
IEC 61249-2-39 : 1ED 2012
$78.00 (-56%) $34.32
Table of Contents
PREFACE
1 INTRODUCTION
1.1 Scope
1.2 Nomenclature
1.3 Common Abbreviations
1.4 Definitions and Terminology
2 BASIC HEAT TRANSFER THEORY
2.1 Conduction
2.2 Radiation
3 SOLAR SYSTEM CONSTANTS
4 SPACECRAFT THERMAL COATINGS
4.1 Ideal Versus Available Materials
4.2 Solar Absorptance
4.3 Surface Emittance
4.4 Measurement of Absorptance and Emittance
5 SPACECRAFT THERMAL BALANCE
5.1 Deep Space Probes
5.2 Satellites
5.3 Total Incident Space Radiation
5.4 Thermal Design
6 TESTING
6.1 Space Simulators
7 MATERIAL DEGRADATION
7.1 Ultraviolet Degradation
7.2 Nuclear Radiation
7.3 Meteoroid Bombardment
8 REFERENCES
Abstract
Provides the means by which first-cut approximations of spacecraft surface, structure, and equipment temperatures may be made, using the curves of planetary and solar heat flux in conjunction with the desired coating radiative properties.
General Product Information
| Document Type | Standard |
| Status | Current |
| Publisher | SAE International |
| Committee | AC-9 |
