04618nam 22008055 450 991036661970332120200705004218.03-030-26965-510.1007/978-3-030-26965-4(CKB)4100000009522846(DE-He213)978-3-030-26965-4(MiAaPQ)EBC6112338(PPN)258061081(EXLCZ)99410000000952284620191010d2020 u| 0engurnn|008mamaatxtrdacontentcrdamediacrrdacarrierChemical Rockets[electronic resource] Performance Prediction and Internal Ballistics Design /by Subramaniam Krishnan, Jeenu Raghavan1st ed. 2020.Cham :Springer International Publishing :Imprint: Springer,2020.1 online resource (XI, 538 p. 23 illus., 2 illus. in color.) Springer Aerospace Technology,1869-17303-030-26964-7 Includes bibliographical references and index.PartI: Performance Calculation of Chemical Propellants by Energy Minimization -- Chapter1: Introduction -- Chapter2: Chemical Potential -- Chapter3: Mass Balance -- Chapter4: Iteration Equations -- Chapter5: Thermodynamic Derivatives -- Chapter6: Thermodynamic Data -- Chapter7: Theoretical Rocket Performance -- PartII: Performance Prediction and Internal Ballistics Design of Solid Propellant Rocket Motors -- Chapter8: Introduction -- Chapter9: Equilibrium–Pressure Analysis -- Chapter10: Incremental Analysis -- Chapter11: Computer Program.The purpose of this book is to discuss, at the graduate level, the methods of performance prediction for chemical rocket propulsion. A pedagogical presentation of such methods has been unavailable thus far and this text, based upon lectures, fills this gap. The first part contains the energy-minimization to calculate the propellant-combustion composition and the subsequent computation of rocket performance. While incremental analysis is for high performance solid motors, equilibrium-pressure analysis is for low performance ones. Both are detailed in the book's second part for the prediction of ignition and tail-off transients, and equilibrium operation. Computer codes, adopting the incremental analysis along with erosive burning effect, are included. The material is encouraged to be used and presented at lectures. Senior undergraduate and graduate students in universities, as well as practicing engineers and scientists in rocket industries, form the readership.Springer Aerospace Technology,1869-1730Aerospace engineeringAstronauticsEngineering designThermodynamicsHeat engineeringHeat transferMass transferFluid mechanicsApplied mathematicsEngineering mathematicsAerospace Technology and Astronauticshttps://scigraph.springernature.com/ontologies/product-market-codes/T17050Engineering Designhttps://scigraph.springernature.com/ontologies/product-market-codes/T17020Engineering Thermodynamics, Heat and Mass Transferhttps://scigraph.springernature.com/ontologies/product-market-codes/T14000Engineering Fluid Dynamicshttps://scigraph.springernature.com/ontologies/product-market-codes/T15044Mathematical and Computational Engineeringhttps://scigraph.springernature.com/ontologies/product-market-codes/T11006Aerospace engineering.Astronautics.Engineering design.Thermodynamics.Heat engineering.Heat transfer.Mass transfer.Fluid mechanics.Applied mathematics.Engineering mathematics.Aerospace Technology and Astronautics.Engineering Design.Engineering Thermodynamics, Heat and Mass Transfer.Engineering Fluid Dynamics.Mathematical and Computational Engineering.629.1Krishnan Subramaniamauthttp://id.loc.gov/vocabulary/relators/aut977516Raghavan Jeenuauthttp://id.loc.gov/vocabulary/relators/autMiAaPQMiAaPQMiAaPQBOOK9910366619703321Chemical Rockets2227051UNINA