Technologies for Rapid Affordable Hypersonic Flight Testing

Award Information
Agency:
Department of Defense
Branch
Air Force
Amount:
$100,000.00
Award Year:
2009
Program:
SBIR
Phase:
Phase I
Contract:
FA8650-09-M-3925
Award Id:
93059
Agency Tracking Number:
F083-179-0348
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
2760 Beverly Dr., #4, Aurora, IL, 60502
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
927258277
Principal Investigator:
DonaldYuhas
President
(630) 236-5901
dyuhas@imsysinc.com
Business Contact:
MarjoriePassini Yuhas
Vice President
(630) 236-5901
myuhas@imsysinc.com
Research Institute:
n/a
Abstract
Innovative measurement methods and instruments are needed to advance the state-of-art of hypersonic flight. Improved thermal transport measurement methods speed development, improve understanding, and enhance our ability to validate analytical models and hardware for numerous propulsion and aeroshell applications. Recent studies have shown that in many hypersonic applications ultrasonic-based temperature and heat flux measurements offer distinct advantages over conventional methods. The transient temperature response is limited only by the velocity of sound and not the thermal mass of the sensor. Measurements can be made remotely, which prevents the disturbance of the measured quantity and removes the sensor from the harsh thermal environment. Measurements can be made without modifying the structure in any way e.g. drilling. In spite of these advantages, ultrasonic thermometry has not found widespread use. One reason for this limited use is the lack of low-cost, compact, dedicated, instrumentation which takes full advantage of the ultrasonic-based methods. In this proposal, we fill this gap by developing and demonstrating a multi-channel ultrasonic-based temperature and heat flux measurement capability. This innovation will be initially applied to boundary layer transition measurements in ground-based experiments, but will have the potential for application in a host of in-flight hypersonic experiments. BENEFIT: Ultrasonic thermometry offers unique capabilities to hypersonic vehicle development. Improved thermal transport measurement methods speed development, improve understanding, and enhance our ability to validate analytical models and hardware for numerous propulsion and aeroshell applications. The non-intrusive nature of the method is particularly attractive for hostile environment encountered in hypersonic flight. The immediate market for this technology is primarily in military applications where there is a need for improved thermal transfer measurement tools to drive the development and evaluation of hypersonic materials and components. In addition to the applications in hypersonic vehicle and propulsion systems, the ultrasonic temperature sensor technology has applications in the areas of space lift, space platform, combustion research, and missiles. There is also a potential commercial market in areas where thermal transport data is needed in relatively inaccessible regions such as combustion chambers, reactors and in some glass molding operations.

* information listed above is at the time of submission.

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