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MARC Record from marc_columbia

Record ID marc_columbia/Columbia-extract-20221130-026.mrc:1988510:5624
Source marc_columbia
Download Link /show-records/marc_columbia/Columbia-extract-20221130-026.mrc:1988510:5624?format=raw

LEADER: 05624cam a2200613 i 4500
001 12515176
005 20220625224434.0
006 m o d
007 cr cnu---unuuu
008 161205s2017 nju ob 001 0 eng d
035 $a(OCoLC)ocn965197044
035 $a(NNC)12515176
040 $aN$T$beng$erda$epn$cN$T$dYDX$dUAB$dMERER$dOCLCQ$dLIP$dCOO$dUWW$dNRC$dBUF$dCEF$dRRP$dZCU$dOCLCQ$dUKOBU$dUMI$dOCLCF$dVLB$dK6U$dCCO$dLOA$dCOCUF$dWRM$dSTF$dVT2$dAU@$dWYU$dLVT$dESU$dUKAHL$dOCLCQ$dOCLCO
019 $a965479786$a965739063$a966396620$a967770943$a985460498$a1229061515
020 $a9781118753880$q(electronic bk.)
020 $a1118753887$q(electronic bk.)
020 $a9781523110513
020 $a1523110511
020 $a1118753917
020 $a9781118753910
020 $z9781118753651
020 $z1118753658
020 $z9781118753910$q(epub)
035 $a(OCoLC)965197044$z(OCoLC)965479786$z(OCoLC)965739063$z(OCoLC)966396620$z(OCoLC)967770943$z(OCoLC)985460498$z(OCoLC)1229061515
037 $aCL0500000854$bSafari Books Online
050 4 $aTL782$b.S8 2016eb
072 7 $aTEC$x009000$2bisacsh
082 04 $a629.47/5$223
049 $aZCUA
100 1 $aSutton, George P.$q(George Paul),$d1920-$eauthor.
245 10 $aRocket propulsion elements /$cGeorge P. Sutton, Oscar Biblarz.
250 $aNinth edition.
264 1 $aHoboken, New Jersey :$bJohn Wiley & Sons Inc.,$c[2017]
300 $a1 online resource
336 $atext$btxt$2rdacontent
337 $acomputer$bc$2rdamedia
338 $aonline resource$bcr$2rdacarrier
504 $aIncludes bibliographical references and index.
588 0 $aPrint version record.
505 0 $aCover; Title Page; Copyright; Contents; Preface; Chapter 1: Classification; 1.1. Duct Jet Propulsion; 1.2. Rocket Propulsion; Chemical Rocket Propulsion; Combinations of Ducted Jet Engines and Rocket Engines; Nuclear Rocket Engines; Electric Rocket Propulsion; Other Rocket Propulsion Concepts; International Rocket Propulsion Effort; 1.3. Applications of Rocket Propulsion; Space Launch Vehicles; Spacecraft; Military and Other Applications; References; Chapter 2: Definitions and Fundamentals; 2.1. Definitions; 2.2. Thrust; 2.3. Exhaust Velocity; 2.4. Energy and Efficiencies.
505 8 $a2.5. Multiple Propulsion Systems2.6. Typical Performance Values; 2.7. Variable Thrust; Symbols; Greek Letters; Problems; References; Chapter 3: Nozzle Theory and Thermodynamic Relations; 3.1. Ideal Rocket Propulsion Systems; 3.2. Summary of Thermodynamic Relations; 3.3. Isentropic Flow through Nozzles; Velocity; Nozzle Flow and Throat Condition; Thrust and Thrust Coefficient; Characteristic Velocity and Specific Impulse; Under- and Overexpanded Nozzles; Influence of Chamber Geometry; 3.4. Nozzle Configurations; Cone- and Bell-Shaped Nozzles; 3.5. Real Nozzles; Boundary Layers; Multiphase Flow.
505 8 $aOther Phenomena and LossesPerformance Correction Factors; Four Performance Parameters; 3.6. Nozzle Alignment; Symbols; Greek Letters; Subscripts; Problems; References; Chapter 4: Flight Performance; 4.1. Gravity-Free Drag-Free Space Flight; 4.2. Forces Acting on a Vehicle in the Atmosphere; 4.3. Basic Relations of Motion; 4.4. Space Flight; Elliptical Orbits; Deep Space; Perturbations; Mission Velocity; 4.5. Space Flight Maneuvers; Reaction Control System; 4.6. Effect of Propulsion System on Vehicle Performance; 4.7. Flight Vehicles; Multistage Vehicles; Stage Separation; Launch Vehicles.
505 8 $a4.8. Military Missiles4.9. Flight Stability; Symbols; Greek Letters; Subscripts; Problems; References; Chapter 5: Chemical Rocket Propellant Performance Analysis; 5.1. Background and Fundamentals; 5.2. Analysis of Chamber or Motor Case Conditions; 5.3. Analysis of Nozzle Expansion Processes; 5.4. Computer-Assisted Analysis; 5.5. Results of Thermochemical Calculations; Greek Letters; Subscripts; Problems; References; Chapter 6: Liquid Propellant Rocket Engine Fundamentals; 6.1. Types of Propellants; 6.2. Propellant Tanks; 6.3. Propellant Feed Systems; Local Pressures and Flows.
505 8 $a6.4. Gas Pressure Feed Systems6.5. Tank Pressurization; Factors Influencing the Required Mass of Pressurizing Gas; Simplified Analysis for the Mass of Pressurizing Gas; 6.6. Turbopump Feed Systems and Engine Cycles; Engine Cycles; 6.7. Rocket Engines for Maneuvering, Orbit Adjustments, or Attitude Control; 6.8. Engine Families; 6.9. Valves and Pipelines; 6.10. Engine Support Structure; Symbols; Subscripts; Problems; References; Chapter 7: Liquid Propellants; 7.1. Propellant Properties; Economic Factors; Performance of Propellants; Common Physical Hazards; Desirable Physical Properties.
520 $aCombining fundamental concepts with industry applications, this unique book provides a practical introduction to rocket propulsion principles, mechanisms, and design as applied to guided missiles, space flight, satellite flight, and more. --$cEdited summary from book.
650 0 $aRocket engines.
650 6 $aMoteurs-fusées.
650 7 $aTECHNOLOGY & ENGINEERING$xEngineering (General)$2bisacsh
650 7 $aRocket engines.$2fast$0(OCoLC)fst01099299
655 4 $aElectronic books.
700 1 $aBiblarz, Oscar,$eauthor.
776 08 $iPrint version:$aSutton, George P. (George Paul), 1920-$tRocket propulsion elements.$bNinth edition.$dHoboken, New Jersey : John Wiley & Sons Inc., [2016]$z9781118753651$w(DLC) 2016031557$w(OCoLC)953576462
856 40 $uhttp://www.columbia.edu/cgi-bin/cul/resolve?clio12515176$zACADEMIC - Aerospace & Radar Technology
852 8 $blweb$hEBOOKS