Solid Rocket Motor Internal Insulation PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Solid Rocket Motor Internal Insulation PDF full book. Access full book title Solid Rocket Motor Internal Insulation by United States. National Aeronautics and Space Administration. Download full books in PDF and EPUB format.
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Rocket engines
Languages : en
Pages : 116
Get Book Here
Book Description
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Rocket engines
Languages : en
Pages : 116
Get Book Here
Book Description
Author: Sherwood E. Twitchell
Publisher:
ISBN:
Category : Insulation (Heat)
Languages : en
Pages : 132
Get Book Here
Book Description
Author: A. Truchot
Publisher:
ISBN:
Category :
Languages : en
Pages : 13
Get Book Here
Book Description
The main purpose of internal insulation is to protect the motor case from the thermal environment of propellant combustion products. Several secondary objectives must also be met. Internal insulation must bond to propellant and case, transmit case strain into propellant and sometimes seal the case. In the first step, the general process of internal insulation design is presented: evaluation of thermal environment, selection of material, thermal and structural analyses. For each phase the different analysis methods are described: aerodynamic, thermal, and structural. The different phases of internal insulation fabrication are also presented: elastomer formulation, fabrication of parts and integration into the motor case.
Author: Franck Cauty
Publisher:
ISBN:
Category :
Languages : en
Pages :
Get Book Here
Book Description
Author: A. Davenas
Publisher: Newnes
ISBN: 0080984754
Category : Technology & Engineering
Languages : en
Pages : 623
Get Book Here
Book Description
This book, a translation of the French title Technologie des Propergols Solides, offers otherwise unavailable information on the subject of solid propellants and their use in rocket propulsion. The fundamentals of rocket propulsion are developed in chapter one and detailed descriptions of concepts are covered in the following chapters. Specific design methods and the theoretical physics underlying them are presented, and finally the industrial production of the propellant itself is explained. The material used in the book has been collected from different countries, as the development of this field has occurred separately due to the classified nature of the subject. Thus the reader not only has an overall picture of solid rocket propulsion technology but a comprehensive view of its different developmental permutations worldwide.
Author: Morton Shorr
Publisher:
ISBN:
Category : Solid propellant rockets
Languages : en
Pages : 370
Get Book Here
Book Description
Author: F. N. Fackrell
Publisher:
ISBN:
Category :
Languages : en
Pages :
Get Book Here
Book Description
Author: George P. Sutton
Publisher: John Wiley & Sons
ISBN: 1118174208
Category : Science
Languages : en
Pages : 657
Get Book Here
Book Description
The definitive text on rocket propulsion—now revised to reflect advancements in the field For sixty years, Sutton's Rocket Propulsion Elements has been regarded as the single most authoritative sourcebook on rocket propulsion technology. As with the previous edition, coauthored with Oscar Biblarz, the Eighth Edition of Rocket Propulsion Elements offers a thorough introduction to basic principles of rocket propulsion for guided missiles, space flight, or satellite flight. It describes the physical mechanisms and designs for various types of rockets' and provides an understanding of how rocket propulsion is applied to flying vehicles. Updated and strengthened throughout, the Eighth Edition explores: The fundamentals of rocket propulsion, its essential technologies, and its key design rationale The various types of rocket propulsion systems, physical phenomena, and essential relationships The latest advances in the field such as changes in materials, systems design, propellants, applications, and manufacturing technologies, with a separate new chapter devoted to turbopumps Liquid propellant rocket engines and solid propellant rocket motors, the two most prevalent of the rocket propulsion systems, with in-depth consideration of advances in hybrid rockets and electrical space propulsion Comprehensive and coherently organized, this seminal text guides readers evenhandedly through the complex factors that shape rocket propulsion, with both theory and practical design considerations. Professional engineers in the aerospace and defense industries as well as students in mechanical and aerospace engineering will find this updated classic indispensable for its scope of coverage and utility.
Author: Ashraf Fathy Ahmed
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Get Book Here
Book Description
Internal insulation in a solid rocket motor is a layer of heat-barrier material placed between the internal surface of the case and the propellant. The primary function of internal insulation is to prevent the rocket motor case from reaching temperatures that may endanger its structural integrity. An extensive experimental and theoretical work in the development and characterization of asbestos-free rubbers for use as rocket motor insulators has been performed. The insulation is based on chopped carbon fiber and/or aramid fiber in the pulp form as fillers for Ethylene Propylene Diene Monomer (EPDM). The first aim of the research is to provide an understanding of the mechanism, the principle, and the process for making polymeric thermal insulants. The second aim is to produce thermal insulants based on polymers with different fillers having different compositions which are capable of working under extreme thermal conditions of 2760 °C (5000 °F). This is through an investigation on the processing, installation, physical, mechanical, thermal and ablative properties of these materials. A hybrid of chopped carbon fiber and Kevlar pulp filled EPDM has been shown to exhibit better thermal, mechanical, physical and ablative properties than its asbestos containing counterpart. Also the prediction of thermal conduction of multiphase thermal insulation composite materials was done using series, parallel, Maxwell Euken and effective medium theory models. Comparison with the measured values allows determining which model estimates best the thermal conductivity of composite insulation material. Development of a suitable optimization technique to reach the best parameters of the selected material was done by doing transient dynamic analysis to determine the response of these materials under a time-varying thermal load. A new type of insulation material using prepregs was developed for the first time. This consists of the development of the prepregs and their assembly to make insulant laminates. This laminate has been shown to exhibit better physical, mechanical, thermal and ablative properties than a hybrid of chopped carbon fiber and Kevlar pulp filled EPDM.
Author: James W. Kordig
Publisher:
ISBN:
Category : Rocket engines
Languages : en
Pages : 112
Get Book Here
Book Description
