NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Metal Matrix Composites for Rocket Engine ApplicationsThis document is from a presentation about the applications of Metal Matrix Composites (MMC) in rocket engines. Both NASA and the Air Force have goals which would reduce the costs and the weight of launching spacecraft. Charts show the engine weight distribution for both reuseable and expendable engine components. The presentation reviews the operating requirements for several components of the rocket engines. The next slide reviews the potential benefits of MMCs in general and in use as materials for Advanced Pressure Casting. The next slide reviews the drawbacks of MMCs. The reusable turbopump housing is selected to review for potential MMC application. The presentation reviews solutions for reusable turbopump materials, pointing out some of the issues. It also reviews the development of some of the materials.
Document ID
20000070411
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
McDonald, Kathleen R.
(Boeing Co. Canoga Park, CA United States)
Wooten, John R.
(Boeing Co. Canoga Park, CA United States)
Date Acquired
September 7, 2013
Publication Date
May 16, 2000
Subject Category
Composite Materials
Meeting Information
Meeting: Society of Automotive Engineers Meeting
Location: Fort Worth, TX
Country: United States
Start Date: May 1, 2000
Funding Number(s)
CONTRACT_GRANT: NCC8-155
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available