Author: V. L. GOODWINPublisher:
ISBN:
Category :
Languages : en
Pages : 23
Book Description
Structural Requirements of Compressor and Fan Blading of Beryllium Composite Materials
Author: V. L. GOODWINBeryllium Science and Technology
Author: Dennis R. FloydPublisher: Springer
ISBN: 1475706685
Category : Science
Languages : en
Pages : 449
Book Description
Nuclear Science Abstracts
Author: Summary of Beryllium Research and Develpment Programs
Author: A. N. AshurstPublisher:
ISBN:
Category : Beryllium
Languages : en
Pages : 56
Book Description
Proceedings
Author: Publisher: National Academies
ISBN:
Category : Beryllium
Languages : en
Pages : 722
Book Description
D M I C Report
Author: Defense Metals Information CenterPublisher:
ISBN:
Category : Metallurgy
Languages : en
Pages : 498
Book Description
Beryllium Composite Structures
Author: James N. KrusosPublisher:
ISBN:
Category : Beryllium
Languages : en
Pages : 336
Book Description
The methods developed for fabrication of Be sheet composite structures are described. Descriptions and performance evaluation are included for a variety of panels fabricated under the contract consisting of Be load bearing panels and porous ceramic heat shields developed to withstand temperatures in excess of 3000 F. Concepts are outlin d defining application of Be-ceramic composites to aerospace vehicle structures. Be sheet fabrication methods and tooling are described and include such processes as cutting, forming, chem-milling, and brazing. Be sheet faces were brazed to a variety of superalloy and stainless steel honeycomb cores. Three basic porous ceramic foams were developed in the heat shield: Al2O3, ZrO2, and SiO2. (Author).
Beryllium Composite Structures
Author: James N. KrusosPublisher:
ISBN:
Category : Beryllium
Languages : en
Pages : 188
Book Description
Design information is presented for Be and ceramic composite structures for re-entry vehicle applications. A summary of materials and process developments for Be panels and heat shield ceramics, analytical evaluations, and discussion of application of insulated structural concepts to re-entry vehicle systems are included. Also included are the results of panel tests in the severe environments of turbojet and ramjet exhausts. Data suitable for preliminary design considerations are presented for three reinforced heat shield ceramic foams: Al203, SiO2, and ZrO2. Be sandwich panels constructed in the course of the program are described with regard to fabrication potential and performance in aerospace structures.
Author: 
Author: