You are here

LOW CTE METAL MATRIX COMPOSITE FITTINGS

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: N/A
Agency Tracking Number: 1704
Amount: $498,230.00
Phase: Phase II
Program: SBIR
Solicitation Topic Code: N/A
Solicitation Number: N/A
Timeline
Solicitation Year: N/A
Award Year: 1986
Award Start Date (Proposal Award Date): N/A
Award End Date (Contract End Date): N/A
Small Business Information
21119 Superior Street
Chatsworth, CA 91311
United States
DUNS: N/A
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Edward C. Supan
 Investigator
 () -
Business Contact
Phone: () -
Research Institution
N/A
Abstract

THIS PHASE I PROGRAM IS DESIGNED TO DEMONSTRATE THE FEASIBILITY OF PRODUCING LIGHTWEIGHT, LOW CTE METAL-MATRIX COMPOSITE FITTINGS OF GRAPHITE-FIBER/ALUMINUM AND TO SHOW BY MECHANICAL AND PHYSICAL-PROPERTY TESTS THAT THE MATERIAL IS USEFUL FOR APPLICATION TO SPACE STRUCTURAL HARDWARE. THE PROGRAM WILL FOCUS ON RECENTLY DEVELOPED DWG (CONTINUOUS GRAPHITE-FIBER/ALUMINUM) AND DWAL-G (CHOPPED GRAPHITE-FIBER/ALUMINUM) MATERIALS USING THORNEL PITCH 55, PITCH 75, AND PITCH 100 FIBER. SIMPLE SHAPES THAT CAN BE VISUALIZED AS REPRESENTATIVE OF REAL FITTINGS OR JOINTS WILL BE PRODUCED TO DEMONSTRATE FEASIBILITY. SPECIMENS FOR PROPERTY TEST WILL BE TAKEN FROM BOTH THE DEMONSTRATION ITEMS AND FROM PREFORM MATERIAL. STRUCTURAL EVALUATION AND PROPERTY-TEST ANALYSIS, ALONG WITH RECOMMENDATIONS FOR PHASE II PROGRAM TASKS, WILL BE INCLUDED IN THE FINAL REPORT.

* Information listed above is at the time of submission. *

US Flag An Official Website of the United States Government