Chemical rockets : performance prediction and internal ballistics design

• 作者： Krishnan, Subramaniam, author.
• 其他作者：
  • Raghavan, Jeenu, author.
  • SpringerLink (Online service)
• 其他題名：
  • Springer aerospace technology.
• 出版： Cham : Springer International Publishing :Imprint: Springer
• 叢書名： Springer aerospace technology,
• 主題： Rockets (Aeronautics)--Fuel. , Rocket engines. , Aerospace Technology and Astronautics. , Engineering Design. , Engineering Thermodynamics, Heat and Mass Transfer. , Engineering Fluid Dynamics. , Mathematical and Computational Engineering.
• ISBN： 9783030269654 (electronic bk.) 、 9783030269647 (paper)
• FIND@SFXID: CGU
• 資料類型: 電子書
• 內容註: 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.
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• 摘要註: 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.
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