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Non-Eroding Fin Materials

Award Information
Agency: Department of Defense
Branch: Army
Contract: N/A
Agency Tracking Number: 32957
Amount: $66,956.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: N/A
Solicitation Number: N/A
Solicitation Year: N/A
Award Year: 1996
Award Start Date (Proposal Award Date): N/A
Award End Date (Contract End Date): N/A
Small Business Information
4300 San Mateo Blvd Ne Suite A220
Albuquerque, NM 87110
United States
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 William M. Congdon
 (303) 795-8106
Business Contact
Phone: () -
Research Institution

This project will analyze and select promising materials and designs to be used in the plumes of tactical solid rocket motors for missile steering and control. The emphasis is on high-performance refractory materials and compatibility of material systems. The control fins experience severe thermal and severe particulate erosion environments. Missile controllability requires fins with minimal erosion and minimal shape change. In Phase I we will study, analyze, and narrow down the list of candidate materials and designs for detailed evaluation and testing in Phase II. Advanced tungsten alloys produced by power metallurgy will be investigated as promising candidates for fin leading edges. Zirconium and hafnium diboride composite-ceramics will also be analyzed. Flank locations on the fin will be studied and here less exotic materials show promise including quartz phenolic and other reinforced and filled, dimensionally-stable, phenolic systems. Phase I is primarily an analysis effort and will rely heavily on well-established analysis methods and tools including SPF, SIRRM, AERHET, TOPAZ, NIKE, SINDA, CMA/ACE, and TCAP.

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

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