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Company Information:

Company Name: APPLIED TECHNOLOGY ASSOC., INC.
City: CORAL SPRINGS
State: FL
Zip+4: 33071
Woman-Owned: No
Minority-Owned: No
HUBZone-Owned: No
Website URL: N/A
Phone: (954) 346-9576

Award Totals:

Program/Phase Award Amount ($) Number of Awards
SBIR Phase I $685,516.00 12
SBIR Phase II $2,381,452.00 5

Award List:

FUTURE NASA SPACECRAFT MAY REQUIRE MEANS TO TRANSPORT THERMAL ENERGY BETWEEN STRUCTURAL MODULES CONNECTED IN ORBIT.

Award Year / Program / Phase: 1984 / SBIR / Phase I
Agency: NASA
Principal Investigator: William clark , INVESTIGATOR
Award Amount: $49,800.00
Abstract:
Future nasa spacecraft may require means to transport thermal energy between structural modules connected in orbit. these modules may be allowed to rotate or gimbal, and the thermal transport system would have to accomodate such motion. a thermal transport system addressing this need would feature a… More

ACTIVE COOLING CONCEPTS FOR REENTRY VEHICLES REVIEW

Award Year / Program / Phase: 1985 / SBIR / Phase I
Agency / Branch: DOD / USAF
Principal Investigator: Robert Cavalleri
Award Amount: $49,662.00

ACTIVE COOLING CONCEPTS FOR REENTRY VEHICLES REVIEW

Award Year / Program / Phase: 1986 / SBIR / Phase II
Agency / Branch: DOD / USAF
Principal Investigator: Robert Cavalleri
Award Amount: $401,000.00
Abstract:
Existing experimental data for active cooling concepts will be reviewed. in particular three concepts will be considered, slot cooling, gas jet nose tip cooling and transpiration cooling. the data reviewed will be screened for use as input and analysis by a time dependent navier stokes computer… More

BASE DRAG ADVERSELY IMPACTS PROJECTILE RANGE.

Award Year / Program / Phase: 1986 / SBIR / Phase I
Agency / Branch: DOD / ARMY
Principal Investigator: Robert cavalleri
Award Amount: $49,797.00
Abstract:
Base drag adversely impacts projectile range. reduction of base drag can lead to improved projectile range. there are several approaches that can potentially be employed to decrease base drag such as base bleed and external burning. a combination of these concepts will be analized using an unsteady… More

THRUST VECTOR CONTROL USING MOVEABLE STRUTS

Award Year / Program / Phase: 1987 / SBIR / Phase I
Agency: NASA
Principal Investigator:
Award Amount: $50,000.00

THRUST VECTOR CONTROL USING MOVEABLE STRUTS

Award Year / Program / Phase: 1988 / SBIR / Phase II
Agency: NASA
Principal Investigator:
Award Amount: $487,000.00
Abstract:
Thrust vector control of solid propellant rocket nozzles canbe obtained with the use of either fluid dynamic means or mechanical means. the fluid dynamic techniques employ injection of gas or liquid into the exhaust nozzle through the nozzle wall. the mechanical techniques employ moving the nozzle… More

ACTIVELY COOLED DECOY NOSETIPS

Award Year / Program / Phase: 1988 / SBIR / Phase I
Agency / Branch: DOD / USAF
Principal Investigator: Dr robert cavalleri
Award Amount: $49,822.00
Abstract:
Cooling concepts for re-entry vehicle nose tips employ either passive ablative techniques or active cooling techniques. ablative techniques cause foreign gas species from the ablation process to be present in the ambient air and effect the aerodynamic performance of the vehicle. the active cooling… More

SUPERSONIC COMBUSTOR ENHANCEMENT STUDY

Award Year / Program / Phase: 1988 / SBIR / Phase I
Agency / Branch: DOD / NAVY
Principal Investigator: Dr robert cavalleri
Award Amount: $49,892.00
Abstract:
The supercomputer has made possible the use of computational fluid dynamics for optimizing the aerodynamics of propulsion system components. this ability will increase even more in the next few years when new supercomputers become operational, permitting complete propulsion systems to be analyzed.… More

LIGHT WEIGHT ROTARY COMPRESSOR EVALUATION FOR ADVANCED MARINE PROPULSION APPLICATIONS

Award Year / Program / Phase: 1990 / SBIR / Phase I
Agency / Branch: DOD / NAVY
Principal Investigator: Dr Robert Cavalleri
Award Amount: $49,687.00

LIGHT WEIGHT ROTARY COMPRESSOR EVALUATION FOR ADVANCED MARINE PROPULSION APPLICATIONS

Award Year / Program / Phase: 1991 / SBIR / Phase II
Agency / Branch: DOD / NAVY
Principal Investigator: Dr Robert Cavalleri
Award Amount: $499,742.00
Abstract:
Rotary compressors are capable of providing larger volumes of compressed gas than reciprocating machines. this is primarily related to the fact that rotary machines can rotate at higher speeds than reciprocating devices. a high efficiency, large displacement rotary compressor offers versatility and… More

FAILURE ENGINEERED HEAVY METAL PENETRATORS

Award Year / Program / Phase: 1992 / SBIR / Phase I
Agency / Branch: DOD / ARMY
Principal Investigator: Dr. Robert Cavalleri
Award Amount: $47,856.00
Abstract:
Tungsten or tungsten alloys are used as penetrators in kinetic energy weapons. used by itself, tungsten is a brittle metal and fractures unless it is alloyed with other metals. typical metals used in tungsten alloys are copper, iron, nichel and silver. they permit the resulting alloy to be machined.… More

REPLACEMENT REFRIGERANT AND SYSTEM EVALUATION

Award Year / Program / Phase: 1992 / SBIR / Phase I
Agency / Branch: DOD / USAF
Principal Investigator: Dr. Robert Cavalleri
Award Amount: $49,965.00

REPLACEMENT REFRIGERANT AND SYSTEM EVALUATION

Award Year / Program / Phase: 1993 / SBIR / Phase II
Agency / Branch: DOD / USAF
Principal Investigator: Dr. Robert Cavalleri
Award Amount: $643,710.00
Abstract:
The current refrigerants used in the vapor cycle systems are scheduled to be phased out and replaced with refrigerants that are environmentally less hazardous. these refrigerants are being developed to replace those currently employed in residential and commercial applications and will also find use… More

Experimental and Analytical Jet Vane Development

Award Year / Program / Phase: 1993 / SBIR / Phase I
Agency / Branch: DOD / NAVY
Principal Investigator: Robert Cavalleri
Award Amount: $69,745.00

Experimental and Analytical Jet Vane Development

Award Year / Program / Phase: 1997 / SBIR / Phase II
Agency / Branch: DOD / NAVY
Principal Investigator: Robert Cavalleri
Award Amount: $350,000.00
Abstract:
The jet vane is located in the aft region of the missile propulsion system nozzle and is used as a Thrust Vector Control device. In order for the jet vane to function properly, it must be designed to survive the thermal and erosive environment of the propulsion system gas stream. An improved jet… More

Suppression of Thermal Emission from Exhaust Components

Award Year / Program / Phase: 2001 / SBIR / Phase I
Agency / Branch: DOD / ARMY
Principal Investigator: Robert Cavalleri, President
Award Amount: $70,000.00
Abstract:
Thermal signatures generated by hot components or hot engine exhaust gases can be suppressed by mixing cool ambient air with the hot component gas stream. In the development of signature reduction concepts, it is desirable to obtain a better understandingof the physical flow processes, hardware… More

Energetic Solid Rocket Nozzle / Throat Insulator Concept

Award Year / Program / Phase: 2001 / SBIR / Phase I
Agency / Branch: DOD / USAF
Principal Investigator: Robert Cavalleri, President
Award Amount: $99,290.00
Abstract:
Throat erosion of rocket nozzles results in lower expansion ratios and reduced specific impulse. The erosion can be minimized or completely eliminated by employing throat cooling to keep the throat material below the throat material critical temperature.Evaluation and fabrication of a cooled… More