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J. S. Shelley


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

Total Results: 5 Results per page:
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Yes - This is Rocket Science: MMCs for Liquid Rocket Engines NOV 2001 34 pages
Authors:  J. S. Shelley; AIR FORCE RESEARCH LAB EDWARDS AFB CA
The full text of this report is available for sale.


Yes--This is Rocket Science: MMCs for Liquid Rocket Engines 05 JUN 2001 49 pages
Authors:  J. S. Shelley; R. LeClaire; D. Miracle; J. Nichols; AIR FORCE RESEARCH LAB EDWARDS AFB CA SPACE AND MISSILE PROPULSION DIV
The full text of this report is available for sale.The Air Force's Integrated High-Payoff Rocket Propulsion Technologies (IHPRPT) Program has established aggressive goals for both improved performance and reduced cost of rocket engines and components. Achieving these goals relies on developing affordable Metal Matrix Composite (MMC) technologies for application to Liquid Rocket Engines (LREs). Efforts are being conducted on three types of MMCs: Aluminum, Copper, and Nickel matrix material systems. Potential applications include turbopump housings, rotating machinery, and high ...


Metal Matrix Composites for Liquid Rocket Engines 25 JAN 2001 16 pages
Authors:  J. S. Shelley; R. LeClaire; J. Nichols; AIR FORCE RESEARCH LAB EDWARDS AFB CA
The full text of this report is available for sale.This article presents an overview of current research and material requirements for Metal Matrix Composite (MMC) technologies being developed for application to Liquid Rocket Engines (LIRE). Developments in LRE technology for the US Air Force are being tracked and planned through the Integrated High Payoff Rocket Propulsion Technologies Program (IHPRPT). Current efforts and research requirements for three types of MMC systems are discussed: Aluminum., Copper and Nickel matrix material systems. ...


Smart Structures for Rocket Propulsion Systems SEP 2000 9 pages
Authors:  J. S. Shelley; AIR FORCE RESEARCH LAB EDWARDS AFB CA
The full text of this report is available for sale.Solid and liquid propellant rocket propulsion systems are weigh- and performance - driven machines whose components experience extreme environments. However, the structural integrity of both types of propulsion systems is currently monitored through type testing, labor-intensive x-ray analysis, and other NDE techniques. Smart structures technologies have the potential not only to alleviate some of the maintenance burden of current rocket propulsion systems but also improve the capability of future systems. ...


Degradation of Nylon-6/Clay Nanocomposites in NO(x) 24 APR 2000 6 pages
Authors:  J. S. Shelley; K. L. Devries; AIR FORCE RESEARCH LAB EDWARDS AFB CA SPACE AND MISSILE PROPULSION DIV
The full text of this report is available for sale.Nylon-6 is an important engineering polymer that, in its fully spherulitic (bulk) form, has many applications in gears, rollers, and other long life cycle components. In 1993, Toyota commercialized a nylon-6/clay nanocomposite out of which it produced the timing belt cover for the 1993 Camry. Although these hybrid nanocomposites show significant improvements in their mechanical response characteristics, including yield strength and heat distortion temperature, little is known about the degradation ...


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