Fundamental Concepts of Liquid-Propellant Rocket Engines

The book includes extensive data on existing engines, typical values for design parameters, and worked-out examples of how the concepts discussed can be applied, helping readers integrate them in their own work. Detailed bibliographical references (including books, articles, and items from the “gray literature”) are provided at the end of each chapter, together with information on valuable resources that can be found online. Given its scope, the book will be of particular interest to undergraduate and graduate students of aerospace engineering.

  • Delivery

    ₹75 shipping all over India

  • Secure Payment

    100% Secure Payment

2,010.004,674.00

In stock

This book is intended for students and engineers who design and develop liquid-propellant rocket engines, offering them a guide to the theory and practice alike. It first presents the fundamental concepts (the generation of thrust, the gas flow through the combustion chamber and the nozzle, the liquid propellants used, and the combustion process) and then qualitatively and quantitatively describes the principal components involved (the combustion chamber, nozzle, feed systems, control systems, valves, propellant tanks, and interconnecting elements).

Weight 1 kg
Dimensions 23 × 15 × 4 cm
Book Author

Alessandro de Iaco Veris

Edition

1st

Format

Paperback

ISBN

9783030547066

Language

English

Pages

756

Publication Year

Publisher

Customer Reviews

There are no reviews yet.

Be the first to review “Fundamental Concepts of Liquid-Propellant Rocket Engines”

Your email address will not be published. Required fields are marked *