NASA SBIR 2012 Solicitation

FORM B - PROPOSAL SUMMARY


PROPOSAL NUMBER: 12-2 A1.01-9814
PHASE 1 CONTRACT NUMBER: NNX13CL11P
SUBTOPIC TITLE: Aviation External Hazard Sensor Technologies
PROPOSAL TITLE: RIDES: Raman Icing Detection System

SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
Michigan Aerospace Corporation
1777 Highland Drive, Suite B
Ann Arbor, MI 48108 - 2285
(734) 975-8777

PRINCIPAL INVESTIGATOR/PROJECT MANAGER (Name, E-mail, Mail Address, City/State/Zip, Phone)
Charles J Richey
crichey@michiganaerospace.com
1777 Highland Drive, Suite B
Ann Arbor, MI 48108 - 2285
(734) 975-8777 Extension :112

CORPORATE/BUSINESS OFFICIAL (Name, E-mail, Mail Address, City/State/Zip, Phone)
John A Dodds
jdodds@michaero.com
1777 Highland Drive, Suite B
Ann Arbor, MI 48108 - 2285
(734) 975-8777 Extension :136

Estimated Technology Readiness Level (TRL) at beginning and end of contract:
Begin: 3
End: 5

Technology Available (TAV) Subtopics
Aviation External Hazard Sensor Technologies is a Technology Available (TAV) subtopic that includes NASA Intellectual Property (IP). Do you plan to use the NASA IP under the award?
No

TECHNICAL ABSTRACT (Limit 2000 characters, approximately 200 words)
Inflight icing of engines and airframe presents a significant hazard to air transport, especially at lower flight elevations during take-off or on approach. Ice accretions on the wings affect the smooth flow required for proper lift. A thin layer of coarse ice can reduce the lift by 30 percent and increase drag by up to 40 percent. In addition, accretions can also reduce the air intake in engines and affect readings from a (heated) Pitot tube. Michigan Aerospace Corporation (MAC) proposes to continue the development of an integrated LIDAR instrument capable of identifying icing conditions while also allowing for air data sensing as well as other hazard detection capabilities. The resulting Raman Icing Detection System (RIDES), when coupled with MAC's optical air data solution, will provide unprecedented situational awareness and aircraft safety. The proposed solution will operate without protrusions into the flow, behind a common flush-mounted window on the skin of the aircraft, mitigating the risk of ice build-up during operation and therefore providing a critical redundancy through dissimilar measurement of air data parameters while greatly enhancing a pilot's awareness of potential icing hazards. MAC will build on its successful Phase I trade-study and design effort through the fabrication and demonstration of a Phase II prototype in an icing wind tunnel.

POTENTIAL NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
An airborne icing condition detection and characterization system, such as RIDES, will have wide applications in the study of the threat icing conditions pose to aircraft. In addition, the system will allow for climate change studies that look at aerosol concentration and distribution, including water vapor/liquid water content, in the atmosphere. There is potential to combine such a system with MAC's optical air data system and turbulence-detection systems into a unified system that would sense both icing conditions and turbulence hazards ahead and report airspeed along with air, temperature and density routinely.

POTENTIAL NON-NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
Outside NASA, military and civil aviation is often affected by icing, sometimes severely (e.g., Comair flight 3272 in 1997, Air France flight 447 in 2009) and the ability to detect these conditions so as to avoid or at least account for them (activating de-icing systems, etc.) would be of tremendous safety value, suggesting a substantial market. Michigan Aerospace Corporation is already working on NASA projects for clear-air turbulence (CAT) detection and volcanic ash detection ahead of an aircraft. Adding SLD to these optical air data system (OADS)-derived capabilities will lead to a powerful suite of optical instruments capable of measuring air data (air speed and direction along with air density and temperature) and warning of icing conditions, volcanic ash and clear-air turbulence, all without protruding into the flow around the aircraft and without ports or probes that can clog with debris or ice up.

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.)
Air Transportation & Safety
Interferometric (see also Analysis)
Lasers (Ladar/Lidar)
Optical/Photonic (see also Photonics)
Ultraviolet
Visible

Form Generated on 03-04-14 13:38