NASA SBIR 2011 Solicitation

FORM B - PROPOSAL SUMMARY


PROPOSAL NUMBER: 11-1 A2.06-8030
SUBTOPIC TITLE: Aerothermodynamics
PROPOSAL TITLE: Precision Surface Temperature Mapping for Heat Shield Testing

SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
Bodkin Design & Engineering
77 Oak St., Suite 201
Newton, MA 02464 - 1460
(617) 795-1968

PRINCIPAL INVESTIGATOR/PROJECT MANAGER (Name, E-mail, Mail Address, City/State/Zip, Phone)
James Daly
jdaly@bodkindesign.com
77 Oak St., Suite 201
Newton, MA 02464 - 1460
(617) 795-1968

Estimated Technology Readiness Level (TRL) at beginning and end of contract:
Begin: 3
End: 4

TECHNICAL ABSTRACT (Limit 2000 characters, approximately 200 words)
Development of hypersonic flight vehicles for airbreathing access to space and for planetary entry poses several design challenges. One of the primary obstacles is the large uncertainty in predictive capability of models of the aerothermal environment to which these vehicles are subjected. A high priority need for the ground test facilities is instruments which enable remote thermal imaging of entry vehicles with high temperature and spatial resolution, and lower uncertainty than the state-of-the art.

Bodkin Design & Engineering (BDE), with our partners Spectral Sciences, Inc (SSI) and Space Computer Corporation (SCC), has demonstrated a Precision Radiometric Surface Temperature (PRST) sensor to perform stand-off measurements of radiatively heated surfaces. We propose to adapt this system to the needs of ground test facilities for testing of hypersonic re-entry vehicles. The sensor will be capable of stand-off imaging of heated surfaces at ranges from 1 to 100+ meters, measuring surface temperatures from 300-4000K, and providing surface temperature maps with spatial resolution of at least 120x120 pixels. Further, the system will operate as a fast snapshot imager, capable of recording surface temperature data at up to 120 frames per second.

POTENTIAL NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
Commercial applications include any that require non-contact measurement of surface temperatures, and in particular, where the optical properties (emissivity) of the surface may not be known. Examples may include monitoring surfaces under laser illumination, measuring metal parts during machining (lathe, mill), measuring the temperature of airfoil leading edges.

POTENTIAL NON-NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
This sensor may be useful to researchers measuring laser damage to materials, and to those analyzing the physics of mechanically induced plastic flow and shear zone evolution.

TECHNOLOGY TAXONOMY MAPPING (NASA's technology taxonomy has been developed by the SBIR-STTR program to disseminate awareness of proposed and awarded R/R&D in the agency. It is a listing of over 100 technologies, sorted into broad categories, of interest to NASA.)
Active Systems
Aerobraking/Aerocapture
Aerodynamics
Analytical Instruments (Solid, Liquid, Gas, Plasma, Energy; see also Sensors)
Analytical Methods
Characterization
Condition Monitoring (see also Sensors)
Diagnostics/Prognostics
Infrared
Lasers (Cutting & Welding)
Lasers (Machining/Materials Processing)
Multispectral/Hyperspectral
Nondestructive Evaluation (NDE; NDT)
Optical/Photonic (see also Photonics)
Passive Systems
Radiometric
Spacecraft Design, Construction, Testing, & Performance (see also Engineering; Testing & Evaluation)
Thermal
Thermal Imaging (see also Testing & Evaluation)


Form Generated on 11-22-11 13:43