You are here

High Temperature Materials for Hypersonic Radomes and Antennas

Award Information
Agency: Department of Defense
Branch: Air Force
Contract: FA8651-19-C-0062
Agency Tracking Number: F18A-013-0102
Amount: $749,999.00
Phase: Phase II
Program: STTR
Solicitation Topic Code: AF18A-T013
Solicitation Number: 18.A
Solicitation Year: 2018
Award Year: 2019
Award Start Date (Proposal Award Date): 2019-06-28
Award End Date (Contract End Date): 2021-06-28
Small Business Information
7800 South Nogales Highway
Tucson, AZ 85756
United States
DUNS: 066066874
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: Yes
Principal Investigator
 Zach Wing
 Director of Science and Technology
 (520) 547-0861
Business Contact
 Mark Angier
Phone: (520) 547-0856
Research Institution
 Villanova University
 Sridhar Santhanam Sridhar Santhanam
800 Lancaster Ave
Villanova, PA 19085
United States

 (610) 519-7924
 Nonprofit College or University

Missiles experience a wide range of thermal and mechanical environments due to the large variety of flight profiles. Since the missile radome is often the aerodynamic leading edge, it undergoes significant thermal and mechanical loading. The radome must survive the dynamic pressure loading, thermal shock and environmental erosion from airborne particulates (rain / sand) while performing as an electromagnetic window through which targeting and tracking is performed. There is no single radome material suitable for all missiles. This is due to the variation in thermal, mechanical, and electrical requirements caused by the variability of missile flight profiles and RF transmission needs. Hence, several radome materials are commonly used. These vary from fused silica, to silicates, oxides, and polycrystalline nitrides. As vehicles and projectiles move to higher speeds and transmission needs push to higher frequencies, new radome , window, and antenna material options are needed. Our research team at Advanced Ceramics Manufacturing and Villanova University proposes new materials be developed based on composite mixtures of ceramics. Based on effective medium theory, our technical approach will engineer the dielectric properties of the radome materials. This will produce high strength, low permittivity, temperature stable materials suitable for hypersonic applications.

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

US Flag An Official Website of the United States Government