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Titlebook: Rocket Propulsion Primer; Subramaniam Krishnan,Jeenu Raghavan Textbook 2024 The Editor(s) (if applicable) and The Author(s), under exclusi

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发表于 2025-3-21 18:05:52 | 显示全部楼层 |阅读模式
书目名称Rocket Propulsion Primer
编辑Subramaniam Krishnan,Jeenu Raghavan
视频video
概述Covers fundamentals of rocket propulsion.Consists of end-of-chapter conceptual questions and numerical problems with answers.Includes biographies of the pioneers in the field
图书封面Titlebook: Rocket Propulsion Primer;  Subramaniam Krishnan,Jeenu Raghavan Textbook 2024 The Editor(s) (if applicable) and The Author(s), under exclusi
描述.This textbook covers fundamentals of rocket propulsion such as history, classification, qualitative design, quantitative design of internal ballistics and rocket vehicle optimization. It is intended to be used as a textbook by the undergraduate/advanced undergraduate students of aerospace engineering. It further describes the classification of aerospace propulsion, two-phase flows, nozzle contour design, advanced nozzle concepts (plug and expansion deflection nozzles) and materials. It also deals with the optimization of multistage rocket vehicles and their trajectories with reference to the currently operational orbital launch vehicles. This textbook contains numerous end-of-chapter problems to aid in self-learning of the students. It will be highly useful for the aerospace and mechanical engineering students. This can also be used as a reference guide by the scientists and engineers working in the areas of aerospace engineering... .
出版日期Textbook 2024
关键词Rocket Propulsion; Rockets Classification; Rocket Design; Internal Ballistics; Orbital Vehicles
版次1
doihttps://doi.org/10.1007/978-981-97-5644-5
isbn_softcover978-981-97-5646-9
isbn_ebook978-981-97-5644-5
copyrightThe Editor(s) (if applicable) and The Author(s), under exclusive license to Springer Nature Singapor
The information of publication is updating

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发表于 2025-3-21 21:19:38 | 显示全部楼层
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Qualitative-Performance and Technology,ow equations for mass-flow rate, velocity, and area ratio are derived. Nozzle-flow separation, maximum thrust, thrust controls, wider altitude operations, and side loads are all considered. Characteristic velocity, thrust coefficient, and ., and their experimental and theoretical values towards engi
发表于 2025-3-22 07:07:25 | 显示全部楼层
Quantitative Internal-Ballistics Prediction and Design,c data of many propellant ingredients and additives are tabled. And, to evaluate the species’ properties ., ., and ., the fourth-order polynomials are introduced along with the coefficients’ values. . The chemical potential . is the unit molar Gibbs energy of species .. Hence, the equilibrium is rea
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Propulsion System Classification, explained. Features of flight-proven electric thrusters are tabled. . For interplanetary travel and beyond by humans, a relatively large power with unlimited energy through nuclear propulsion is the requirement. . Number of concept questions and numerical problems with answers are included at the chapter end.
发表于 2025-3-23 03:02:53 | 显示全部楼层
发表于 2025-3-23 09:04:26 | 显示全部楼层
Qualitative-Performance and Technology,zzles are discussed. . Polymeric materials, composites, and structural as well as high-temperature alloys, and their applications in the construction of solid and liquid rockets are considered. . Under the sections worked examples and at the end a large number of concept questions and numerical problems with answers are included.
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