Storming Media: Pentagon Reports and DocumentsPentagon Reports: Fast. Definitive. Complete.     
New Account »
Forgot Password?
Advanced Search »

Newsletter
Unsubscribe »
Reports by Author

Roberto J. Cano


Click on the titles below to find US government-authored or -collected reports written by Roberto J. Cano

Total Results: 3 Results per page:
Sort by: Title Date Desc Pages Display:
Double Lap Shear Testing of Coating-Modified Ice Adhesion to Specific Shuttle Component Surfaces DEC 2006 62 pages
Authors:  Michael G. Ferrick; Nathan D. Mulherin; Barry A. Coutermarsh; Glenn D. Durell; Leslie A. Curtis; Terry L. St. Clair; Erik S. Weiser; Roberto J. Cano; Trent M. Smith; Charles G. Stevenson; Eloy C. Martinez; ENGINEERING RESEARCH AND DEVELOPMENT CENTER HANOVER NH COLD REGIONS RESEARCH AND ENGINEERING LAB
The full text of this report is available for sale.The goals of this experimental program were to optimize the effectiveness of an icephobic coating for use on several Space Shuttle surfaces, to evaluate the effects of adding an ultraviolet light absorber (UVA) on coating performance, and to assess the consistency and durability of the basic coating and its modifications. The double lap shear test was used to quantify ice adhesion performance at a constant temperature of 112 C ( ...


Evaluation of the Mechanical Properties and Damage Tolerance of Five New Toughened Matrix Composite Materials, 12 MAR 1992
Authors:  Roberto J. Cano; Marvin B. Dow; NATIONAL AERONAUTICS AND SPACE ADMINISTRATION HAMPTON VA LANGLEY RESEARCH CEN TER
The full text of this report is not available and therefore is not for sale. This information is provided for reference purposes only.The notched and unnotched tension and compression properties of quasi-isotropic laminates, and compression after impact strengths of five carbon fiber/toughened matrix composites, (IM7/E7T1-2, IM7/X1845, G40-800X/5255-3, IM7/5255-3, and IM7/5260) were evaluated. The compression after impact (CAI) strengths were determined primarily by impacting quasi-isotropic laminates with a 1.27-cm diameter aluminum projectile fired from an air gun. A few CAI tests were also made using a drop weight impactor. For a given impact ...


Evaluation of the Mechanical Properties and Damage Tolerance of Five New Toughened Matrix Composite Materials. 1992
Authors:  Roberto J. Cano; Marvin B. Dow; NATIONAL AERONAUTICS AND SPACE ADMINISTRATION HAMPTON VA LANGLEY RESEARCH CEN TER
The full text of this report is not available and therefore is not for sale. This information is provided for reference purposes only.The use of toughened matrix composite materials offers a potentially attractive solution to the problem of poor damage tolerance associated with aircraft composite materials. In this study, the notched tension and compression properties of quasi-isotropic laminates, and compres- sion after after impact strengths of five carbon fiber/toughened matrix composites, IM7/E7T1-2, IM7/X1845, G40-800X/5255-3, IM7/5255-3, and IM7/5260, have been evaluated. The compression after impact (CAI) strengths were determined primarily by impacting quasi-isotropic ...


Total Results: 3 Results per page: