Spacecraft Thermal Control, Design and Operation
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20

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2

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Published By American Institute Of Aeronautics And Astronautics

9780915928750, 9781600865596

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Table Of Contents

Spacecraft Thermal Control, Design and Operation ◽

10.2514/5.9781600865596.0000.0000 ◽

1983 ◽

pp. i-xxvi

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Control-Volume-Based Finite-Element Formulation Of The Heat Conduction Equation

Spacecraft Thermal Control, Design and Operation ◽

10.2514/5.9781600865596.0305.0327 ◽

1983 ◽

pp. 305-327 ◽

Cited By ~ 2

Keyword(s):

Finite Element ◽

Heat Conduction ◽

Heat Conduction Equation ◽

Control Volume ◽

Conduction Equation ◽

Finite Element Formulation ◽

Element Formulation

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The Marangoni Effect In Axially Grooved Variable-Conductance Heat Pipes

Spacecraft Thermal Control, Design and Operation ◽

10.2514/5.9781600865596.0222.0238 ◽

1983 ◽

pp. 222-238

Keyword(s):

Marangoni Effect ◽

Heat Pipes ◽

Variable Conductance Heat Pipes

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Thermodynamic Optimization Of A Cryogenic Storage System For Minimum Boiloff

Spacecraft Thermal Control, Design and Operation ◽

10.2514/5.9781600865596.0130.0146 ◽

1983 ◽

pp. 130-146

Keyword(s):

Storage System ◽

Thermodynamic Optimization ◽

Cryogenic Storage

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Satellite Thermal Design And Analyses For Expendable And Shuttle Launch Environments

Spacecraft Thermal Control, Design and Operation ◽

10.2514/5.9781600865596.0089.0106 ◽

1983 ◽

pp. 89-106

Keyword(s):

Thermal Design

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Author Index

Spacecraft Thermal Control, Design and Operation ◽

10.2514/5.9781600865596.0345.0345 ◽

1983 ◽

pp. 345-345

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The Thermal Contact Conductance Of Dissimilar Metals

Spacecraft Thermal Control, Design and Operation ◽

10.2514/5.9781600865596.0266.0277 ◽

1983 ◽

pp. 266-277

Keyword(s):

Thermal Contact ◽

Thermal Contact Conductance ◽

Dissimilar Metals ◽

Contact Conductance

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Design, Fabrication, And Test Of Liquid-Metal Heat-Pipe Sandwich Panels

Spacecraft Thermal Control, Design and Operation ◽

10.2514/5.9781600865596.0165.0181 ◽

1983 ◽

pp. 165-181

Keyword(s):

Liquid Metal ◽

Heat Pipe ◽

Sandwich Panels

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Molecular Absorption Crygenic Cooler For Liquid Hydrogen Propulsion Systems

Spacecraft Thermal Control, Design and Operation ◽

10.2514/5.9781600865596.0147.0162 ◽

1983 ◽

pp. 147-162

Keyword(s):

Liquid Hydrogen ◽

Molecular Absorption ◽

Propulsion Systems

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Development Of A Double-Wall Artery High-Capacity Heat Pipe

Spacecraft Thermal Control, Design and Operation ◽

10.2514/5.9781600865596.0202.0221 ◽

1983 ◽

pp. 202-221 ◽

Cited By ~ 3

Keyword(s):

Heat Pipe ◽

High Capacity ◽

Double Wall

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