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|n Title subscribed to via ProQuest Academic Complete
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|a dlr
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|b .P75 vol. 29
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|a 629.47/01/5367
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|a UAMI
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| 245 |
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|a Fundamentals of spacecraft thermal design
|c Edited by John W. Lucas.
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| 260 |
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|a Cambridge, Mass.,
|b MIT Press
|c [1972]
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| 300 |
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|a 1 online resource (xvi, 599 pages)
|b illustrations
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| 336 |
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|a text
|b txt
|2 rdacontent
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| 337 |
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|a computer
|b c
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|a online resource
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|a data file
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| 490 |
1 |
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|a Progress in astronautics and aeronautics,
|v v. 29
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| 504 |
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|a Includes bibliographical references.
|
| 588 |
0 |
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|a Print version record.
|
| 506 |
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|3 Use copy
|f Restrictions unspecified
|2 star
|5 MiAaHDL
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| 533 |
|
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|a Electronic reproduction.
|b [Place of publication not identified] :
|c HathiTrust Digital Library,
|d 2010.
|5 MiAaHDL
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| 538 |
|
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|a Master and use copy. Digital master created according to Benchmark for Faithful Digital Reproductions of Monographs and Serials, Version 1. Digital Library Federation, December 2002.
|u http://purl.oclc.org/DLF/benchrepro0212
|5 MiAaHDL
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| 583 |
1 |
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|a digitized
|c 2010
|h HathiTrust Digital Library
|l committed to preserve
|2 pda
|5 MiAaHDL
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| 505 |
0 |
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|a 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
|
| 505 |
8 |
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|a 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
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| 505 |
8 |
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|a 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
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| 505 |
8 |
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|a 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
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| 505 |
8 |
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|a 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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| 546 |
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|a English.
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| 590 |
|
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|a ProQuest Ebook Central
|b Ebook Central Academic Complete
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| 650 |
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0 |
|a Space vehicles
|x Thermodynamics
|v Congresses.
|
| 650 |
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6 |
|a Véhicules spatiaux
|x Thermodynamique
|v Congrès.
|
| 650 |
|
7 |
|a Space vehicles
|x Thermodynamics.
|2 fast
|0 (OCoLC)fst01128098
|
| 655 |
|
7 |
|a Conference papers and proceedings.
|2 fast
|0 (OCoLC)fst01423772
|
| 700 |
1 |
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|a Lucas, John W.,
|d 1923-
|e editor.
|
| 711 |
2 |
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|a AIAA Aerospace Sciences Meeting
|n (9th :
|d 1971 :
|c New York, N.Y.)
|
| 711 |
2 |
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|a AIAA Thermophysics Conference
|n (6th :
|d 1971 :
|c Tullahoma, Tenn.)
|
| 776 |
0 |
8 |
|i Print version:
|t Fundamentals of spacecraft thermal design.
|d Cambridge, Mass., MIT Press [1972]
|z 0262120593
|z 9780262120593
|w (DLC) 72005605
|w (OCoLC)354305
|
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|
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|a Progress in astronautics and aeronautics ;
|v v. 29.
|
| 856 |
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|u https://ebookcentral.uam.elogim.com/lib/uam-ebooks/detail.action?docID=3111676
|z Texto completo
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