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Modern Engineering for Design of Liquid Propellant Rocket Engines (Progress in Astronautics and Aeronautics)
 
 
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Modern Engineering for Design of Liquid Propellant Rocket Engines (Progress in Astronautics and Aeronautics) [Hardcover]

Dieter K. Huzel (Author), David H. Huang (Author), Rocketdyne Divisi D. Huzel and D. Huang (Author)
4.6 out of 5 stars  See all reviews (9 customer reviews)

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Book Description

1563470136 978-1563470134 January 1992 Rev Sub
From the component design, to the subsystem design, to the engine systems design, engine development and flight-vehicle application, this how-to text bridges the gap between basic physical and design principles and actual rocket-engine design as it's done in industry. More than 470 illustrations and tables should make this book a must-read for advanced students and engineers active in all phases of engine systems design, development and application in industry and in government agencies.

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Product Details

  • Hardcover: 431 pages
  • Publisher: AIAA (American Institute of Aeronautics & Ast; Rev Sub edition (January 1992)
  • Language: English
  • ISBN-10: 1563470136
  • ISBN-13: 978-1563470134
  • Product Dimensions: 11.2 x 8.7 x 1.2 inches
  • Shipping Weight: 2.3 pounds (View shipping rates and policies)
  • Average Customer Review: 4.6 out of 5 stars  See all reviews (9 customer reviews)
  • Amazon Best Sellers Rank: #369,686 in Books (See Top 100 in Books)

 

Customer Reviews

9 Reviews
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Average Customer Review
4.6 out of 5 stars (9 customer reviews)
 
 
 
 
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14 of 14 people found the following review helpful:
5.0 out of 5 stars the best., February 7, 2006
This review is from: Modern Engineering for Design of Liquid Propellant Rocket Engines (Progress in Astronautics and Aeronautics) (Hardcover)
i have most of the books on rocket engines that are sold today.
i must say that this is the best book about DESIGN of LIQUID ROCKET ENGINES: if you want to design a LRE, this book gives to you a chance. it's QUITE easy to read, taking in consideration that the topic is very complicate. consider that i'm a computer science university student, and i have no problem in understanding it. this book is about DESIGN, LIQUID ROCKET and ENGINES: so if you are interested in general infos about rockets, missile guidance, solid rocket, apollo on moon, illustrated books about missiles and rockets, cold war secrets etc., you are out of the way.i reported this obvious consideration because sometimes "an AMAZONer" buy some engineering book for his 5 years child and, being the son less than a genius, give to the book 1 star because he lost his money OR, since he doesn't read entirely the title of the book, he thinks that the book is something of *erotic*.

this book is an improvement of the huzel's "st-125" NASA's book, one of the first book used to introduce rocket design elements to nasa's workers when no textbooks on this topic were available. if you already have the st-125, probably you'll find "some" informations redundant. i have also the st-125. i know that
you can find this book for less, but i suggest you to buy "modern engineering.." because st-125 is a '71 pubblication,
and its perspective on liquid rockets engines is 35 years old, and 21 years older; in addition, it is a perspective that not consider the progresses of the nineties: after the end of the cold war, american engineers could collect benefits by the disclosing of russian tecnologies, and this changed some trends in aerospace.
remember that if you know little about rockets but you have a scientific background, there are better books for you. try first the sutton's "rocket propulsion elements" or "Rocket and Spacecraft Propulsion : Principles, Practice and New Developments" by Martin (but i think the first of the two is better worth the price).

i think that the only things that can be improved is the exposition of detailed infos about high pressure rocket engines,
that is to say staged combustion cycle rockets. the most powerful (thrust/weight ratio speaking) engines were all closed cycle engines(including space shuttle's SSME,russian moon rocket's nk-33,atlas' rd-180).

i'm waiting (if possible) for a newer edition of this book. i'd buy it for sure.
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16 of 18 people found the following review helpful:
5.0 out of 5 stars The best book on the subject!, June 7, 2000
By A Customer
This review is from: Modern Engineering for Design of Liquid Propellant Rocket Engines (Progress in Astronautics and Aeronautics) (Hardcover)
The book "Modern Engineering for Design Liquid Propellant Rocket Engines" is undoubtedly the best book on liquid fueled rockets. The information is not just valuable, it is priceless. Few textbooks of any subject go as much into detail as this book. Do NOT question the price. The value of the information given in this book goes way beyond the price tag. If you are interested in learning the aspects of this subject, or want to build your own rocket engine, this book is definitely for you.
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10 of 12 people found the following review helpful:
5.0 out of 5 stars Great liquid rocket engine book, July 13, 2001
This review is from: Modern Engineering for Design of Liquid Propellant Rocket Engines (Progress in Astronautics and Aeronautics) (Hardcover)
This is a very well written reference book and is packed full of useful information. I work in liquid propulsion design and I have been able to find very detailed subsystem information. Well worth the price.
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Inside This Book (learn more)
Key Phrases - Statistically Improbable Phrases (SIPs): (learn more)
bulging stress, propellant flowrates, pressurant weight, valve pressure drop psi, nozzle expansion area ratio, weight flowrate, cylindrical tank section, overall engine system performance, prestart conditioning, regulated outlet pressure, engine thrust chamber, main oxidizer tank, main oxidizer valve, coax element, cutoff impulse, bipropellant gas generator, gimbal plane, seating closures, bleed regulator, engine mixture ratio, slipper seal, injector face, main propellant valves, main thrust chamber, nozzle stagnation pressure
Key Phrases - Capitalized Phrases (CAPs): (learn more)
New York, Air Force, Space Shuttle Orbiter, San Antonio, Machine Design, Overall Diameter, Helium Helium, High Velocity Duct Systems, Study of Minimum Pressure Loss, High Fair Very, Journal of Basic Engineering, Product Engineering, Quarterly Rep, East Launch, Post Launch
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