Fundamentals of spacecraft thermal design / / edited by John W. Lucas

• Pubblicazione: Cambridge, Mass., : MIT Press, [1972]
• Edizione: 1st ed.
• Descrizione fisica: xvi, 599 p. : ill
• Disciplina: 629.47/01/5367; 629.1/08 s
• Soggetto topico: Space vehicles - Thermodynamics
• Altri autori: LucasJohn W
• Note generali: "Technical papers selected from the AIAA 9th Aerospace Sciences Meeting, January 1971, and the AIAA 6th Thermophysics Conference, April 1971, subsequently revised for this volume."
• Nota di bibliografia: Includes bibliographical references and index.
• Nota di contenuto: 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 -- Particulate Radiation Effects on the Solar Absorptance of Thermal Control Surfaces -- Long-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 Material -- Study 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 Analyses -- Spacecraft 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 Control -- A 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 -- M -- N -- P -- S -- T -- W -- Y -- Z.
• Titolo autorizzato: Fundamentals of spacecraft thermal design
• ISBN: 1-60086-503-8; 1-60086-284-5
• Formato: Materiale a stampa
• Livello bibliografico: Monografia
• Lingua di pubblicazione: Inglese
• Record Nr.: 9911094981203321
• Lo trovi qui: Univ. Federico II
• Serie: Progress in astronautics and aeronautics ; ; v. 29.