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Radiation Resistant, Reconfigurable, Shape Memory Metal Rubber Space Arrays

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNX10RA85P
Agency Tracking Number: 090080
Amount: $100,000.00
Phase: Phase I
Program: STTR
Solicitation Topic Code: T3
Solicitation Number: N/A
Timeline
Solicitation Year: N/A
Award Year: 2010
Award Start Date (Proposal Award Date): N/A
Award End Date (Contract End Date): N/A
Small Business Information
1485 South Main Street
Blacksburg, VA 24060
United States
DUNS: 008963758
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Jennifer Lalli
 Principal Investigator
 (540) 953-1785
 jlalli@nanosonic.com
Business Contact
 Lisa B. Lawson
Title: Contracts Administrator
Phone: (540) 953-1785
Research Institution
 Colorado State University
 
1618 Campus Delivery
Ft. Collins, CO 80523
United States

 (970) 491-6450
 Nonprofit College or University
Abstract

NanoSonic has demonstrated that Shape Memory Metal RubberTM (SM-MR) adaptive skins exhibit reconfigurable and durable RF properties. It is hypothesized that such morphing skins shall also exhibit durable radiation resistance upon morphing; a property that few, if any, flexible materials offer. Typical highly filled or metal evaporated nanocomposites crack and spall upon flexation, and cannot be repeatedly mechanically stretched without rupture after a few cyclic strains. SM-MR nanostructured morphing materials are based on self-assembled high z, dense, Au and Ag nanoparticles, rather than Pb. Our manufacturing process yields tough skins that can be repeatedly and severely mechanically morphed without loss of EMI shielding (-88dB). NanoSonic, together with Colorado State University, have demonstrated that SM-MR is up to 50% lighter in weight and provides greater gamma ray attenuation relative to commercial off-the-shelf shielding materials, without emitting harmful secondary radiation under a 137Cs source. During Phase I, radiation shielding would be verified for SM-MR during potential disparate space array morphed configurations to demonstrate durability, stowability, and reconfigurability for space tolerant structures with self-healing properties to reach TRL6. TRL8 and 9 shall be reached during Phase II and III with assistance from our space systems prime partner upon flight testing and integration.

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

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