- Type: Hardcover Book.
- Publisher: AIAA (American Institute of Aeronautics & Astronautics)
- Language : English
Modern Engineering for Design of Liquid Propellant Rocket Engines by Dieter K. Huzel and David H. Huang (ISBN 9781563470134)
Modern Engineering for Design of Liquid Propellant Rocket Engines by Dieter K. Huzel and David H. Huang is the definitive engineering guide to the design, development, and operation of liquid rocket propulsion systems. Published as part of the Progress in Astronautics and Aeronautics series by the American Institute of Aeronautics and Astronautics (AIAA), this book remains an essential reference for aerospace engineers and propulsion specialists worldwide.
Product Details
- Title: Modern Engineering for Design of Liquid Propellant Rocket Engines
- Series: Progress in Astronautics and Aeronautics
- Edition: Revised, Subsequent Edition
- Authors: Dieter K. Huzel, David H. Huang
- Publisher: AIAA (American Institute of Aeronautics and Astronautics)
- ISBN-13: 9781563470134
- Format: Hardcover / Technical Reference
- Pages: 432 +
- Price: $69.99
- Availability: In Stock | Free Worldwide Shipping
Based on decades of propulsion engineering experience, this book presents a complete overview of liquid rocket engine design, analysis, and manufacturing. It covers the evolution of rocket engines, detailed system components, and design methodologies used in NASA and industry programs. The content serves both as a reference manual and a practical engineering guide for modern propulsion development.
Key Features of the Revised Edition
- Comprehensive Design Guidance: Covers combustion chambers, injectors, pumps, valves, regulators, and cooling systems.
- Performance Analysis: Detailed treatment of thrust equations, mixture ratios, and thermodynamic cycles.
- Component-Level Engineering: Includes case studies on turbopumps, gas generators, and pressurization systems.
- Materials and Manufacturing: Discussion on high-temperature alloys, coatings, and fabrication for rocket systems.
- Testing and Reliability: Procedures for static testing, failure analysis, and operational safety validation.
- Historical and Modern Context: References to both classic NASA designs and contemporary commercial applications.
Table of Contents Highlights
- Introduction to Liquid Rocket Propulsion
- Fundamentals of Combustion and Performance
- Engine System Design and Configuration
- Injector and Combustion Chamber Design
- Feed Systems, Turbopumps, and Valves
- Cooling and Thermal Management
- Control Systems and Instrumentation
- Testing, Reliability, and Flight Qualification
Who Should Use This Book?
- Aerospace engineers and propulsion designers
- Graduate students in astronautics or mechanical engineering
- Rocket and satellite development professionals
- Researchers in combustion and propulsion systems
- Space industry contractors and system integrators
Why Buy from BooksGoat?
- Best Price: $69.99 vs $90+ retail
- Free Worldwide Shipping
- Authentic AIAA Publication: Verified Revised Edition (Progress in Astronautics & Aeronautics Series)
- Eco-Friendly Packaging: Durable, sustainable shipping worldwide
FAQs
- Does this edition include modern rocket engine data?
- Yes — it includes updated design approaches, materials, and performance equations relevant to current liquid propulsion systems.
- Is it suitable for academic and professional use?
- Absolutely — it’s a standard reference for both university coursework and aerospace industry training.
- Are SpaceX-style systems discussed?
- While written before newer commercial systems, its engineering principles apply directly to modern cryogenic and staged-combustion engines.
Final Call – Buy Now
Modern Engineering for Design of Liquid Propellant Rocket Engines by Dieter K. Huzel and David H. Huang is the benchmark reference in rocket propulsion engineering. Order now from BooksGoat for $69.99. Free worldwide shipping included.
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