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Company Information:

Company Name:
High Technology Corporation
Address:
28 Research Drive
Hampton, VA 23666
Phone:
(757) 865-0818
URL:
N/A
EIN:
541179831
DUNS:
N/A
Number of Employees:
6
Woman-Owned?:
No
Minority-Owned?:
Yes
HUBZone-Owned?:
No

Commercialization:

Has been acquired/merged with?:
N/A
Has had Spin-off?:
N/A
Has Had IPO?:
N/A
Year of IPO:
N/A
Has Patents?:
N/A
Number of Patents:
N/A
Total Sales to Date $:
$ 0.00
Total Investment to Date $
$ 0.00
POC Title:
N/A
POC Name:
N/A
POC Phone:
N/A
POC Email:
N/A
Narrative:
N/A

Award Totals:

Program/Phase Award Amount ($) Number of Awards
SBIR Phase I $1,756,016.00 27
SBIR Phase II $5,688,627.00 10
STTR Phase I $100,000.00 1

Award List:

STABILITY AND TRANSITION IN CHEMICALLY REACTING NONEQUILIBRIUM FLOWS

Award Year / Program / Phase:
1988 / SBIR / Phase I
Award Amount:
$50,608.00
Agency / Branch:
DOD / DARPA
Principal Investigator:
Dr mujeeb r malik
Abstract:
It is proposed here to develop a method for prediction of transition on nasp (national aero-space plane) configuration and for the control/enhancement of supersonic combustion in the scramjet. the method is based upon linear stability analysis with noneequilibrium effects which typify the boundary… More

NUMERICAL AND ANALYTIAL STUDIES OF LAMINAR TO TURBULENCE TRANSITION

Award Year / Program / Phase:
1989 / SBIR / Phase I
Award Amount:
$49,920.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Dr Mujeeb R Malik
Abstract:
N/a

NUMERICAL AND ANALYTIAL STUDIES OF LAMINAR TO TURBULENCE TRANSITION

Award Year / Program / Phase:
1990 / SBIR / Phase II
Award Amount:
$179,309.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Dr Mujeeb R Malik
Abstract:
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… More

ADVANCED COMPUTATIONAL TECHNIQUES IN STUDIES OF HYPERSONIC BOUNDARY-LAYER TRANSITION

Award Year / Program / Phase:
1990 / SBIR / Phase I
Award Amount:
$49,994.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Mujeeb R Malik
Abstract:
The objective of the proposed work is to use advanced theoretical and computational techniques for studies of hypersonic boundary layer stability and transition to turbulence. these studies will enhance our understanding of the transition phenomena and thus help predict and control transition with a… More

Transition Prediction and Laminar Flow Control in Compressible 3D Boundary Layers Using PSE

Award Year / Program / Phase:
1993 / SBIR / Phase I
Award Amount:
$49,927.00
Agency:
NASA
Principal Investigator:
Mujeeb R. Malik
Abstract:
N/a

Transistion Control in Corner Flow of a Supersonic Square Nozzle

Award Year / Program / Phase:
1994 / SBIR / Phase I
Award Amount:
$67,548.00
Agency:
NASA
Principal Investigator:
Ray-Sing Lin
Abstract:
"Quiet" (low-disturbance) wind tunnels, needed for transitionresearch, require cleverly designed nozzle contours forstabilization or delay of dominant instabilities in supersonicnozzle wall boundary layers. However, if a nozzle of squarecross-section

Drag-Prediction Algorithms for Navier-Stokes Solutions over Single- and Multi-Element Airfoils

Award Year / Program / Phase:
1994 / SBIR / Phase I
Award Amount:
$68,760.00
Agency:
NASA
Principal Investigator:
Paul M. Vijgen
Abstract:
Accurate prediction of the aerodynamic lift and drag is acritical requirement in the development process of an aircraft.Presently, computational methods based on numerical solution ofthe Reynolds-averaged Navier-Stokes (N-S) equations are beingapplie

Active Suppression of Resonance Interactions between Shear-Layers and Cavities

Award Year / Program / Phase:
1994 / SBIR / Phase I
Award Amount:
$68,801.00
Agency:
NASA
Principal Investigator:
Richard W. Wlezien
Abstract:
N/a

Supersonic Jet-Noise Prediction and Control

Award Year / Program / Phase:
1994 / SBIR / Phase I
Award Amount:
$68,458.00
Agency:
NASA
Principal Investigator:
Ponnampalam Balakumar
Abstract:
N/a

Transition Prediction and Laminar Flow Control in Compressible 3D Boundary Layers Using PSE

Award Year / Program / Phase:
1994 / SBIR / Phase II
Award Amount:
$485,880.00
Agency:
NASA
Principal Investigator:
Mujeeb R. Malik
Abstract:
N/a

Active Suppression of Resonance Interactions between Shear-Layers and Cavities

Award Year / Program / Phase:
1995 / SBIR / Phase II
Award Amount:
$599,767.00
Agency:
NASA
Principal Investigator:
Richard W. Wlezien
Abstract:
The control of the resonant interaction between a free shearlayer and an open cavity is of direct relevance to wind-tunneltesting and aircraft applications. Techniques will beinvestigated for the control of acoustic resonances in opencavity flows. Th

Supersonic Jet-Noise Prediction and Control

Award Year / Program / Phase:
1995 / SBIR / Phase II
Award Amount:
$598,302.00
Agency:
NASA
Principal Investigator:
Ponnampalam Balakumar
Abstract:
Recent studies have demonstrated that a definite relation existsbetween instability waves and noise of high-speed jets and,hence, the instability wave model can be used to predict certainfeatures of the jet noise. The instability model used in theses

Optimization Of Suction For Laminar Flow Control Applications

Award Year / Program / Phase:
1995 / SBIR / Phase I
Award Amount:
$67,822.00
Agency:
NASA
Principal Investigator:
Jamal A. Masad , Research Scientist
Abstract:
N/a

Prediction and Active Control of Flow-Induced Weapons Bay Acoustics

Award Year / Program / Phase:
1995 / SBIR / Phase I
Award Amount:
$79,653.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Louis N. Cattafesta, Iii
Abstract:
N/a

Active Control/Alleviation Of Trailing (Streamwise) Vortices

Award Year / Program / Phase:
1995 / SBIR / Phase I
Award Amount:
$68,821.00
Agency:
NASA
Principal Investigator:
Mehdi R. Khorrami , Research Scientist
Abstract:
N/a

Prediction and Active Control of Flow-Induced Weapons Bay Acoustics

Award Year / Program / Phase:
1996 / SBIR / Phase II
Award Amount:
$737,215.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Louis N. Cattafesta, Iii
Abstract:
The modeling and active control of the resonant interaction between a free shear layer and an open cavity is of direct relevance to military aircraft applications. Techniques will be investigated to first model and then control acoustic resonance in open cavity flows. The problem consists of the… More

HYBRID LAMINAR FLOW CONTROL TECHNIQUE FOR ENGINE NACELLES

Award Year / Program / Phase:
1996 / SBIR / Phase I
Award Amount:
$69,910.00
Agency:
NASA
Principal Investigator:
Jamal A. Masad , Research Scientist
Abstract:
N/a

A PROGRAMMING ENVIRONMENT FOR THE DEVELOPMENT OF LARGE SCIENTIFIC SYSTEMS ON A DISTRIBUTED COMPUTING NETWORK

Award Year / Program / Phase:
1996 / SBIR / Phase I
Award Amount:
$69,894.00
Agency:
NASA
Principal Investigator:
Thomas M. Eidson , Senior Scientist
Abstract:
N/a

Optimization Of Suction For Laminar Flow Control Applications

Award Year / Program / Phase:
1996 / SBIR / Phase II
Award Amount:
$587,826.00
Agency:
NASA
Principal Investigator:
Jamal A. Masad , Research Scientist
Abstract:
N/a

LAMINAR-TURBULENT TRANSITION PREDICTION OF REACTING FLOWS IN HYPERSONIC VEHICLES APPLICATION

Award Year / Program / Phase:
1996 / SBIR / Phase I
Award Amount:
$68,868.00
Agency:
NASA
Principal Investigator:
Chau-lyan Chang , Research Scientist
Abstract:
N/a

A Novel Computational Tool For Hypersonic Transition Prediction

Award Year / Program / Phase:
1997 / SBIR / Phase I
Award Amount:
$67,032.00
Agency:
NASA
Principal Investigator:
Mujeeb R. Malik , CHIEF SCIENTIST
Abstract:
N/a

A PROGRAMMING ENVIRONMENT FOR THE DEVELOPMENT OF LARGE SCIENTIFIC SYSTEMS ON A DISTRIBUTED COMPUTING NETWORK

Award Year / Program / Phase:
1997 / SBIR / Phase II
Award Amount:
$570,483.00
Agency:
NASA
Principal Investigator:
Thomas M. Eidson , Senior Scientist
Abstract:
N/a

LAMINAR-TURBULENT TRANSITION PREDICTION OF REACTING FLOWS IN HYPERSONIC VEHICLES APPLICATION

Award Year / Program / Phase:
1997 / SBIR / Phase II
Award Amount:
$580,103.00
Agency:
NASA
Principal Investigator:
Chau-lyan Chang , Research Scientist
Abstract:
N/a

Advanced Actuator Systems for Separation Control

Award Year / Program / Phase:
1998 / SBIR / Phase I
Award Amount:
$100,000.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Louis N. Cattafesta, Iii
Abstract:
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… More

A Novel Computational Tool for Transition Prediction over Hypersonic Vehicles

Award Year / Program / Phase:
1998 / SBIR / Phase I
Award Amount:
$100,000.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Mujeeb R. Malik
Abstract:
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… More

Advanced Prediction Tool for Simulation of Turbomachinery Noise Sources

Award Year / Program / Phase:
1998 / SBIR / Phase I
Award Amount:
$70,000.00
Agency:
NASA
Principal Investigator:
Abstract:
N/a

An advanced system for dynamic model deformation and angle-of-attack measurements

Award Year / Program / Phase:
1998 / SBIR / Phase I
Award Amount:
$70,000.00
Agency:
NASA
Principal Investigator:
Abstract:
N/a

Control and Alteration of Wing-Tip Flowfield for Induced Drag Reduction

Award Year / Program / Phase:
1998 / SBIR / Phase I
Award Amount:
$70,000.00
Agency:
NASA
Principal Investigator:
Abstract:
N/a

A Novel Approach for Mitigation of Rotor Tip-Clearance Induced noise in Turbofan Engines

Award Year / Program / Phase:
1999 / SBIR / Phase I
Award Amount:
$70,000.00
Agency:
NASA
Principal Investigator:
Mehdi R. Khorrami, Senior Scientist
Abstract:
N/a

High-Lift Transition Prediction Module

Award Year / Program / Phase:
1999 / SBIR / Phase I
Award Amount:
$70,000.00
Agency:
NASA
Principal Investigator:
Ray-Sing Lin, Research Scientist
Abstract:
N/a

A Lifetime Pressure Sensitive Paint (PSP) and Model Deformation Imaging System

Award Year / Program / Phase:
1999 / SBIR / Phase I
Award Amount:
$70,000.00
Agency:
NASA
Principal Investigator:
Louis N. Cattafesta III, Senior Research Scientist
Abstract:
N/a

N/A

Award Year / Program / Phase:
2000 / SBIR / Phase I
Award Amount:
$100,000.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Mujeeb R. Malik, Chief Scientist
Abstract:
N/a

A Photogrammetric Imaging System for Measurement of Flight Control Surfaces

Award Year / Program / Phase:
2001 / SBIR / Phase I
Award Amount:
$70,000.00
Agency:
NASA
Principal Investigator:
Deepak Shukla, Research Scientist
Abstract:
The development of a commercially viable photogrammetric system is proposed for measurement of motion and deformation of flight control surfaces. This system will measure the position, velocity and deformation of flight control surfaces in an aircraft where such deformation typically includes… More

USAT: Unified Software for Analysis of Transition

Award Year / Program / Phase:
2002 / SBIR / Phase II
Award Amount:
$759,742.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Mujeeb R. Malik, Chief Scientist
Abstract:
"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 forcedesigners to be conservative by adding weight… More

A Real-Time Photogrammetric Imaging System for Flight Control Surfaces

Award Year / Program / Phase:
2002 / SBIR / Phase I
Award Amount:
$0.00
Agency:
NASA
Principal Investigator:
Deepak Shukla, Research Scientist
Abstract:
The development of a commercially viable photogrammetric system is proposed for measurement of motion and deformation of flight control surfaces. This system will measure the position, velocity and deformation of flight control surfaces in an aircraft where such deformation typically includes… More

A Real-Time Photogrammetric Imaging System for Flight Control Surfaces

Award Year / Program / Phase:
2002 / SBIR / Phase II
Award Amount:
$590,000.00
Agency:
NASA
Principal Investigator:
Deepak Shukla, Research Scientist
Abstract:
The development of a commercially viable photogrammetric system is proposed for measurement of motion and deformation of flight control surfaces. This system will measure the position, velocity and deformation of flight control surfaces in an aircraft where such deformation typically includes… More

USAT: Unified Software for Analysis of Transition

Award Year / Program / Phase:
2002 / SBIR / Phase I
Award Amount:
$0.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Mujeeb R. Malik, Chief Scientist
Abstract:
"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 forcedesigners to be conservative by adding weight… More