Rocket Propulsion Elements: An Introduction to the Engineering of RocketsA revision of the standard text on the basic technology, performance and design rationale of rocket propulsion. After discussing fundamentals, such as nozzle thermodynamics, heat transfer, flight performance and chemical reaction analysis, the book continues with treatments of various types of liquid and solid propellants and rocket testing. It brings together the engineering science disciplines necessary for rocket design: thermodynamics, heat transfer, flight mechanics, chemical reactions and materials behavior. SI units and information on computer-aided testing have also been added. |
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Innehåll
Classification | 1 |
Definitions and Fundamentals | 21 |
Nozzle Theory and Thermodynamic Relations | 35 |
Upphovsrätt | |
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Rocket Propulsion Elements: An Introduction to the Engineering of Rockets George Paul Sutton Fragmentarisk förhandsgranskning - 1986 |
Vanliga ord och fraser
acceleration actual altitude applications average burning rate calculated cause chamber pressure Chapter characteristics chemical coefficient combustion chamber common composition constant coolant cooling correction determined devices diameter effective energy Equation example exhaust exhaust velocity expansion Figure flight flow fluid force fuel function gases give given grain heat transfer hydrogen ideal ignition increase initial injection injector liquid propellant loading losses m/sec mass material maximum missile mixture ratio motor nozzle operation orbit oxidizer oxygen performance propellant rocket properties propulsion pump range reaction Reference relatively rocket engine separate shown solid propellant space spacecraft specific heat ratio specific impulse speed stage stress surface Table tank temperature throat thrust chamber tion turbine types typical unit usually valve vehicle volume wall weight
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