You are here

Integrated Sensors for the Evaluation of Structural Integrity of Inflatable Habitats

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNX16CL60P
Agency Tracking Number: 150187
Amount: $125,000.00
Phase: Phase I
Program: STTR
Solicitation Topic Code: T12.03
Solicitation Number: N/A
Timeline
Solicitation Year: 2016
Award Year: 2016
Award Start Date (Proposal Award Date): 2016-06-10
Award End Date (Contract End Date): 2017-06-09
Small Business Information
158 Wheatland Drive
Pembroke, VA 24136-3645
United States
DUNS: 000000000
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Michelle Berg
 Principal Investigator
 (540) 626-6266
 mberg@nanosonic.com
Business Contact
 Melissa Campbell
Title: CFO
Phone: (540) 626-6266
Email: mcampbell@nanosonic.com
Research Institution
 Virginia Tech
 Melissa Campbell
 
302 Whittemore
Blacksburg, VA 24061-0000
United States

 (540) 626-6266
 Domestic Nonprofit Research Organization
Abstract

Future long-duration, crewed space habitat systems will be inflatable structures. This type of structure is advantageous in that it is not limited to the diameter of the launch vehicle and can therefore provide a greater volume of living and work space. Unlike conventional metal structures, however, softbody inflatables require support members to maintain their desired shapes. Despite their robustness, the webbings strain due to the internal habitat inflation pressure and resulting stress. To measure the relatively large strains that occur in the webbings during the inflation of model habitats used during the design process, pin or clip-on extensometers are used, but the pins damage the material and are unacceptable. Strain sensors directly integrated into or onto low-strain webbing fabrics like Dyneema, Vectran would allow the determination of webbing loads during the inflation process as well as during the use lifetime of the habitat. Such webbing-integrated elongation sensors would have two primary uses. First, they would be used to determine and map mechanical loads during the inflation process to insure that the habitat attains proper design form. Second, in the long-term, they would be used to monitor the gradual creep of the webbings that must be balanced by inflation forces to maintain proper figure.
The purpose of the proposed program is to address this specific NASA need - to develop fabric extensometers that can be built into habitat webbings during their manufacture and used to measure loads during inflation and long-term use. To that end, NanoSonic will build on its Metal Rubber? (MR?) technology to create fabric sensor materials that are electrically conductive and mechanically flexible, tailored to the required performance metrics of the structural webbing materials.

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

US Flag An Official Website of the United States Government