High Technology Corp.

28 Research Drive
Hampton, VA 23666
http://www.htc-tech.com
23 Employees

SBIR Award Summary

Total Number of Awards 11
Total Value of Awards $2.3MM
First Award Date 01/01/88
Most Recent Award Date 09/30/02

Key Personnel

Last Name Name Awards Contact
Malik Dr. Mujeeb R. Malik 8 Message
Cattafesta Louis N. Cattafesta III 3
Choudhari Meelan Choudhari 1

11 Awards Won

Phase 2 SBIR

Agency: Air Force
Topic: AF00-280
Budget: 09/30/02 - 10/30/04

Laminar-Turbulent transition phenomenon in hypersonic flows remains poorly understood although it has a profound impact on the thermal protection system weight, vehicle drag and air-breathing engine performance. Transition location uncertainties force designers to be conservative by adding weight and reducing thrust. Efficient techniques for p...

Phase 1 SBIR

Agency: Air Force
Topic: AF00-280
Budget: 05/16/00 - 03/16/01

Laminar-Turbulent transition phenomenon in hypersonic flows remains poorly understood although it has a profound impact on the thermal protection system weight, vehicle drag and air-breathing engine performance. Transition location uncertainties force designers to be conservative by adding weight and reducing thrust. Efficient techniques for p...

Phase 1 STTR

Institution: University of Florida

Agency: Air Force
Topic: AF99T007
Budget: 08/20/99 - 08/20/00

A strategy is proposed to characterize, model, and develop adaptive feedback control algorithms suitable for nonlinear cavity oscillations. The Phase I effort focuses on the characterization of cavity oscillations via detailed analyses of previously obtained experimental data and companion CFD modeling of the nonlinear phenomenon. These efforts ...

Phase 1 SBIR

Agency: Air Force
Topic: AF98-174
Budget: 04/09/98 - 02/09/99

The development of actuators suitable for boundary-layer separation control is proposed. The Phase I effort focuses on the analysis, design, fabrication, and benchtop testing of prototype systems. The actuators will generate disturbances that are large enough to significantly influence the performance of a high-lift system but will be energy e...

Phase 1 SBIR

Agency: Air Force
Topic: AF98-174
Budget: 04/09/98 - 02/09/99

Laminar to turbulent transition phenomenon in hypersonic flows remains poorly understood although it has a profound impact on the thermal protection system weight, vehicle drag and air-breathing engine performance. Transition location uncertainty forces designers to be conservative by adding weight and reducing thrust. Accurate prediction tech...

Phase 2 SBIR

Agency: Air Force
Topic: AF95-147
Budget: 08/02/96 - 08/02/98

This research addresses techniques for active suppression of pressure oscillations in an open cavity. Flow over an open cavity, as in an aircraft weapons bay, can cause excessive sound pressure levels that lead to failure of system components. Passive suppression techniques can only be optimized for a single condition; thus, and active co...

Phase 1 SBIR

Agency: Air Force
Topic: AF95-147
Budget: 04/12/95 - 11/19/95

Phase 2 SBIR

Agency: Air Force
Topic: AF89-236
Budget: 12/15/90 - 12/15/92

IT IS PROPOSED HERE TO STUDY NONLINEAR DEVELOPMENT OF GORTLER AND CROSSFLOW VORTICES AND INVESTIGATE VARIOUS WAVE-INTERACTION MECHANISMS OPERATIVE IN TWO AND THREE-DIMENSIONAL BOUNDARY LAYERS. THE PROPOSED WORK WILL NUMERICALLY SIMULATE TRANSITION IN A THREEDIMENSIONAL BOUNDARY LAYER. THE OBJECTIVE OF THE RESEARCH IS TO FURTHER THE UNDERSTANDIN...

Phase 1 SBIR

Agency: Air Force
Topic: AF90-095
Budget: 01/01/90 - 12/31/90

Phase 1 SBIR

Agency: Air Force
Topic: AF89-236
Budget: 01/01/89 - 12/31/89

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