Fundamental Concepts of Liquid-Propellant Rocket Engines
Home > General > Fundamental Concepts of Liquid-Propellant Rocket Engines
Fundamental Concepts of Liquid-Propellant Rocket Engines

Fundamental Concepts of Liquid-Propellant Rocket Engines


     0     
5
4
3
2
1



Available


About the Book

Preface

Chapter 1: Fundamental concepts on liquid-propellant rocket

engines

1. The generation of thrust

2. The gas flow through the combustion chamber and the nozzle

3. Performance indicators

4. Liquid propellants for high-thrust rocket engines

5. Combustion of propellants in steady state

6. Combustion of propellants in unsteady state

7. The principal components of a liquid-propellant rocket engine

Chapter 2: The thrust chamber assembly

1. The principal components of a thrust chamber

2. The design of a thrust chamber for thrust vector control

3. Performance of a thrust chamber

4. Configuration and design of a thrust chamber

5. Cooling of a thrust chamber

6. Injectors

7. Gas-generator and other engine cycles

8. Igniters

9. Combustion instability

Chapter 3: Feed systems using gases under pressure

1. Fundamental concepts

2. Requirements for gases stored under pressure

3. Feed systems using gases stored for bi-propellants

4. Feed systems using evaporation of two propellants

5. Feed systems using gases stored for mono-propellants

6. Feed systems using combustion products

7. Control systems for liquid-propellant gas generators

8. Feed systems using direct injection into the main propellant tanks

9. Choice of a feed system using gases under pressure

Chapter 4: Feed systems using turbo-pumps

1. Fundamental concepts

2. Pumps for propellants

3. Turbines driving the pumps

4. Sources of energy for turbines

5. Description of a typical turbo-pump

6. Turbo-pump performance

7. Turbo-pump design parameters

8. Heads and mass flow rates of pumps

9. Design of centrifugal-flow pumps

10. Design of axial-flow pumps

11. Design of turbines

12. Bearings for turbo-pumps

13. Seals for turbo-pumps

14. Gears for turbo-pumps

Chapter 5: Control systems and valves

1. Fundamental concepts on control systems

2. Control systems for rocket engines

3. Control of thrust magnitude

4. Control of propellant mixture ratio

5. Control of propellant consumption

6. Control of thrust direction

7. Principal components of flow control systems

8. Static and dynamic seals for leakage control in valves

9. Design of propellant valves

10. Design of pilot valves

11. Design of flow regulating devices of the fixed-area type

12. Design of servo-valves

13. Design of pressure-reducing regulators

14. Design of differential pressure regulators

15. Design of relief valves

16. Design of check valves

17. Design of burst discs

18. Design of explosive valves

Chapter 6: Tanks for propellants

1. Fundamental concepts

2. Tanks subject only to membrane stresses

3. Tanks subject to membrane and bending stresses

4. Multi-element tanks

5. Tanks subject to loads due to propellant sloshing

6. Slosh-suppression devices for tanks

7. Materials, processes, and environmental conditions of tanks

8. Fracture control of metals used for tanks

9. Structural elements of tanks

Chapter 7: Interconnecting components and structures

1. Fundamental concepts

2. Interconnecting ducts and structures in a rocket engine

3. Materials used for tubing in rocket engines

4. Coupling components for tubing

5. Control of pressure loss in tubing

6. Control of vibrations at the inlet of pumps

7. Bellows joints

8. Flexible hoses

9. Filters

10. Design of a flange joint

11. Gaskets and other seals for flange joints

12. Design of a bellows joint for a flexible
About the Author:

Alessandro de Iaco Veris holds degrees in civil engineering and aerospace engineering, both from the University of Rome. He has also completed specialist training, including a high-level professional course on "Projet, calcul et emploi des fusées spatiales" at the Ecole Nationale Supérieure de l'Aéronautique et de l'Espace (ENSAE) and a course on "Dynamics of Controlled Structures" at Massachusetts Institute of Technology (MIT). He is a strong proponent of the application of mathematics for practical purposes and in particular for the solution of problems arising in engineering. His expertise is in the fields of mathematical models and numerical methods for aerodynamics, space flight mechanics, system studies, and mission analysis. His professional interests include numerical integration methods used to predict the motion of space vehicles and Earth satellites subject to perturbations.


Best Sellers



Product Details
  • ISBN-13: 9783030547035
  • Publisher: Springer International Publishing
  • Publisher Imprint: Springer
  • Height: 234 mm
  • No of Pages: 747
  • Series Title: Springer Aerospace Technology
  • Weight: 1278 gr
  • ISBN-10: 3030547035
  • Publisher Date: 05 Nov 2020
  • Binding: Hardback
  • Language: English
  • Returnable: Y
  • Spine Width: 40 mm
  • Width: 156 mm


Similar Products

Add Photo
Add Photo

Customer Reviews

REVIEWS      0     
Click Here To Be The First to Review this Product
Fundamental Concepts of Liquid-Propellant Rocket Engines
Springer International Publishing -
Fundamental Concepts of Liquid-Propellant Rocket Engines
Writing guidlines
We want to publish your review, so please:
  • keep your review on the product. Review's that defame author's character will be rejected.
  • Keep your review focused on the product.
  • Avoid writing about customer service. contact us instead if you have issue requiring immediate attention.
  • Refrain from mentioning competitors or the specific price you paid for the product.
  • Do not include any personally identifiable information, such as full names.

Fundamental Concepts of Liquid-Propellant Rocket Engines

Required fields are marked with *

Review Title*
Review
    Add Photo Add up to 6 photos
    Would you recommend this product to a friend?
    Tag this Book Read more
    Does your review contain spoilers?
    What type of reader best describes you?
    I agree to the terms & conditions
    You may receive emails regarding this submission. Any emails will include the ability to opt-out of future communications.

    CUSTOMER RATINGS AND REVIEWS AND QUESTIONS AND ANSWERS TERMS OF USE

    These Terms of Use govern your conduct associated with the Customer Ratings and Reviews and/or Questions and Answers service offered by Bookswagon (the "CRR Service").


    By submitting any content to Bookswagon, you guarantee that:
    • You are the sole author and owner of the intellectual property rights in the content;
    • All "moral rights" that you may have in such content have been voluntarily waived by you;
    • All content that you post is accurate;
    • You are at least 13 years old;
    • Use of the content you supply does not violate these Terms of Use and will not cause injury to any person or entity.
    You further agree that you may not submit any content:
    • That is known by you to be false, inaccurate or misleading;
    • That infringes any third party's copyright, patent, trademark, trade secret or other proprietary rights or rights of publicity or privacy;
    • That violates any law, statute, ordinance or regulation (including, but not limited to, those governing, consumer protection, unfair competition, anti-discrimination or false advertising);
    • That is, or may reasonably be considered to be, defamatory, libelous, hateful, racially or religiously biased or offensive, unlawfully threatening or unlawfully harassing to any individual, partnership or corporation;
    • For which you were compensated or granted any consideration by any unapproved third party;
    • That includes any information that references other websites, addresses, email addresses, contact information or phone numbers;
    • That contains any computer viruses, worms or other potentially damaging computer programs or files.
    You agree to indemnify and hold Bookswagon (and its officers, directors, agents, subsidiaries, joint ventures, employees and third-party service providers, including but not limited to Bazaarvoice, Inc.), harmless from all claims, demands, and damages (actual and consequential) of every kind and nature, known and unknown including reasonable attorneys' fees, arising out of a breach of your representations and warranties set forth above, or your violation of any law or the rights of a third party.


    For any content that you submit, you grant Bookswagon a perpetual, irrevocable, royalty-free, transferable right and license to use, copy, modify, delete in its entirety, adapt, publish, translate, create derivative works from and/or sell, transfer, and/or distribute such content and/or incorporate such content into any form, medium or technology throughout the world without compensation to you. Additionally,  Bookswagon may transfer or share any personal information that you submit with its third-party service providers, including but not limited to Bazaarvoice, Inc. in accordance with  Privacy Policy


    All content that you submit may be used at Bookswagon's sole discretion. Bookswagon reserves the right to change, condense, withhold publication, remove or delete any content on Bookswagon's website that Bookswagon deems, in its sole discretion, to violate the content guidelines or any other provision of these Terms of Use.  Bookswagon does not guarantee that you will have any recourse through Bookswagon to edit or delete any content you have submitted. Ratings and written comments are generally posted within two to four business days. However, Bookswagon reserves the right to remove or to refuse to post any submission to the extent authorized by law. You acknowledge that you, not Bookswagon, are responsible for the contents of your submission. None of the content that you submit shall be subject to any obligation of confidence on the part of Bookswagon, its agents, subsidiaries, affiliates, partners or third party service providers (including but not limited to Bazaarvoice, Inc.)and their respective directors, officers and employees.

    Accept

    New Arrivals



    Inspired by your browsing history


    Your review has been submitted!

    You've already reviewed this product!