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Record Nr. |
UNINA9910826065303321 |
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Titolo |
Thermal-hydraulics for space power, propulsion, and thermal management system design [[electronic resource] /] / edited by William J. Krotiuk |
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Pubbl/distr/stampa |
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Washington, D.C., : American Institute of Aeronautics and Astronautics, c1990 |
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ISBN |
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1-60086-596-8 |
1-60086-377-9 |
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Descrizione fisica |
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1 online resource (348 p.) |
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Collana |
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Progress in astronautics and aeronautics ; ; v. 122 |
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Altri autori (Persone) |
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Disciplina |
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Soggetti |
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Space vehicles - Design and construction |
Space vehicles - Thermodynamics |
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Lingua di pubblicazione |
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Formato |
Materiale a stampa |
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Livello bibliografico |
Monografia |
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Note generali |
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Description based upon print version of record. |
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Nota di bibliografia |
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Includes bibliographical references and index. |
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Nota di contenuto |
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""Cover""; ""Title""; ""Copyright""; ""Table of Contents""; ""Preface""; ""Chapter 1. Overview of Thermal-Hydraulic Aspects of Current Space Projects""; ""Space Station Thermal Management Systems""; ""Thermal Design of the Space Station Free-Flying Platforms""; ""SP-100 Space Reactor Power System""; ""Advanced Multimegawatt Space Nuclear Power Concepts""; ""Propulsion Systems""; ""Chapter 2. Space Station Two-Phase Thermal Management""; ""Space Station Mechanical Pumped Loop""; ""Capillary Pumped Loop Supporting Technology"" |
""Chapter 3. Startup Thaw Concept for the SP-100 Space Reactor Power System""""Chapter 4. Calculational Methods and Experimental Data for Microgravity Conditions""; ""Chapter 5. Isothermal Gas-Liquid Flow at Reduced Gravity""; ""Chapter 6. Vapor Generation in Aerospace Applications""; ""Low-Gravity Flow Boiling""; ""Computation of Space Shuttle High-Pressure Cryogenic Turbopump Ball Bearing Two-Phase Coolant Flow""; ""Chapter 7. Reduced-Gravity Condensation""; ""Author Index"" |
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