Rocket Propulsion Elements: An Introduction to the Engineering of RocketsWiley, 1986 - 361 sidor A 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. |
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 altitude applications area ratio attitude control axial burning rate chamber pressure Chapter chemical combustion chamber composite coolant cooling jacket density diameter energy Equation expansion feed system flight flow rate fluid ft/sec fuel gases gravity heat transfer heat-transfer hybrid rocket hydrazine hydrogen ignition injection injector inlet liquid oxygen liquid propellant liquid propellant rocket liquid rocket m/sec mass flow rate material maximum missile mixture ratio monopropellant nozzle exit nozzle throat operation orbit oxidizer parameters particles performance pressure drop pressure ratio propellant flow propellant grain propellant mass propellant rocket engines propulsion system psia pump reaction Reference rocket motor rocket propulsion satellite shown in Figure solid propellant solid propellant rockets solid rocket specific heat specific heat ratio specific impulse stress surface Table thermal throat area thrust coefficient thrust vector tion turbine turbopump types typical UDMH usually valve vapor vehicle weight
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