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Company Information:

Company Name: Atss Inc.
City: San Bernardino
State: CA
Zip+4: 92412
Woman-Owned: No
Minority-Owned: No
HUBZone-Owned: No
Website URL: N/A
Phone: N/A

Award Totals:

Program/Phase Award Amount ($) Number of Awards
SBIR Phase I $910,733.00 17
SBIR Phase II $3,344,828.00 7

Award List:

FRATRICIDE EFFECTS ON ANTENNA BORESIGHT ERRORS

Award Year / Program / Phase: 1987 / SBIR / Phase I
Agency / Branch: DOD / DTRA
Principal Investigator: Henry l moody
Award Amount: $49,942.00
Abstract:
The guidance and surveilllance accuracies of advanced air force reentry systems depend on antenna window shape change (or ablation) at the time of the guidance update or surveillance function. guidance update and surveillance occur in altitude regimes where precursor dust fields can exist. dust… More

HEATSHIELD/STRUCTURE ATTACHMENT

Award Year / Program / Phase: 1987 / SBIR / Phase I
Agency / Branch: DOD / USAF
Principal Investigator: Henry l moody
Award Amount: $54,546.00
Abstract:
Design methods and material combinations shall be identified to enhance the structural integrity of advanced strategic systems using large antenna windows. the integration of antenna windows and heatshields in maneuvering vehicles shall be specifically addressed in the proposed program.

BRILLIANT GUIDANCE FOR ICBMS

Award Year / Program / Phase: 1987 / SBIR / Phase I
Agency / Branch: DOD / USAF
Principal Investigator: Henry L Moody
Award Amount: $63,109.00

ANTENNA WINDOW ABLATION

Award Year / Program / Phase: 1987 / SBIR / Phase I
Agency / Branch: DOD / USAF
Principal Investigator: Henry L Moody
Award Amount: $59,818.00

LOW IMPULSE-HIGH STRENGTH HEATSHIELD

Award Year / Program / Phase: 1988 / SBIR / Phase I
Agency / Branch: DOD / DTRA
Principal Investigator: Henry l moody
Award Amount: $49,994.00
Abstract:
High altitude nuclear threats generally require the use of overlays/underlays to achieve the nuclear survivability requirements of advanced reentry vehicles (rvs). materials and fabrication processes exist that with some minor variations should produce a heatshield material that can either eliminate… More

HYGROSCOPIC EFFECTS ON REENTRY VEHICLE ANTENNA WINDOWS

Award Year / Program / Phase: 1988 / SBIR / Phase I
Agency / Branch: DOD / USAF
Principal Investigator: Henry l moody
Award Amount: $49,988.00
Abstract:
Advanced-high accuracy air force reentry systems can involve the use of electrically steerable antennas to conduct guidance, surveillance and acquisition functions. to achieve the accurary necessary for these system, laboratory tuning at simulated operational conditions is required to prevent errors… More

REENTRY VEHICLE WINDOW SYSTEM DESIGN

Award Year / Program / Phase: 1988 / SBIR / Phase I
Agency / Branch: DOD / USAF
Principal Investigator: Henry L Moody
Award Amount: $53,844.00

TRANSPIRATION COOLED NOSETIP DESIGN TECHNIQUES

Award Year / Program / Phase: 1988 / SBIR / Phase I
Agency / Branch: DOD / USAF
Principal Investigator: Henry L Moody
Award Amount: $55,587.00

BRILLIANT GUIDANCE FOR ICBMS

Award Year / Program / Phase: 1989 / SBIR / Phase II
Agency / Branch: DOD / USAF
Principal Investigator: Henry L Moody
Award Amount: $749,058.00
Abstract:
Brilliant guidance systems for icbms will rely on advanced thermal protection and processing technologies to preserve sensor performance in severe reentry environments. in this study reentry effects on sensors will be assessed, and passive and active thermal protection systems will be evaluated.… More

ANTENNA WINDOW ABLATION

Award Year / Program / Phase: 1989 / SBIR / Phase II
Agency / Branch: DOD / USAF
Principal Investigator: Henry L Moody
Award Amount: $697,497.00
Abstract:
Transient three-dimensional analysis methods shall be added to the couple code (a current air force antenna window ablation analysis method) to predict antenna window/heatshield shape change for maneuvering reentry vehicles. the analysis method shall consider both monolithic and button array antenna… More

HIGH TEMPERATURE INSULATOR

Award Year / Program / Phase: 1989 / SBIR / Phase I
Agency / Branch: DOD / USAF
Principal Investigator: Henry L Moody
Award Amount: $59,716.00
Abstract:
The purpose of the phase i program is to develop an improved aeroshell design for strategic reentry vehicles. the improved design uses a high strength heatshield material that can also provide a structural role in the aeroshell. analyses and ground tests show that the material has equivalent thermal… More

DEVELOPMENT OF A HEATSHIELD

Award Year / Program / Phase: 1989 / SBIR / Phase I
Agency / Branch: DOD / USAF
Principal Investigator: Henry L Moody
Award Amount: $59,578.00
Abstract:
The purpose of the phase i program is to develop design methods and materials for the improvement of strategic reentry vehicle heatshield/substructure capabilities to result in increased strength and/or reduced weight. the integration of large microwave antenna window assemblies in both ballistic… More

IMPROVED STRENGTH CARBON-CARBON FACEPLATE HEATSHIELD FOR PHASED ARRAY ANTENNA WINDOWS

Award Year / Program / Phase: 1989 / SBIR / Phase I
Agency / Branch: DOD / USAF
Principal Investigator: Liam S Groener
Award Amount: $49,988.00
Abstract:
Sensor systems for hypersonic reentry systems can require large arrays which must operate in severe heating environments for long durations. in some designs, these arrays are protected from the environment by individual dielectric windows over each array element, with a high temperature structural… More

HYBRID COWL LEADING EDGE FOR HYPERSONIC FLIGHT SYSTEMS

Award Year / Program / Phase: 1989 / SBIR / Phase I
Agency / Branch: DOD / USAF
Principal Investigator: Henry L Moody
Award Amount: $49,993.00

REENTRY VEHICLE WINDOW SYSTEM DESIGN

Award Year / Program / Phase: 1990 / SBIR / Phase II
Agency / Branch: DOD / USAF
Principal Investigator: Henry L Moody
Award Amount: $134,500.00
Abstract:
The deficiencies in current antenna window materials and design methods restrict the performance goals of certain advanced air force systems. to improve the performance and/or experimental evaluation of antenna windows and therefore improve overall system effectiveness; material formulations,… More

TRANSPIRATION COOLED NOSETIP DESIGN TECHNIQUES

Award Year / Program / Phase: 1990 / SBIR / Phase II
Agency / Branch: DOD / USAF
Principal Investigator: Henry L Moody
Award Amount: $749,845.00
Abstract:
Transpiration cooled nosetips (tcnts) for icbm reentry vehicles offer shape stability, enhanced thermal/erosion performance and potential design solutions for high strength and small radius nosetips. current tcnt design and fabrication processes are time-consuming and expensive, hampering research… More

HYBRID COWL LEADING EDGE FOR HYPERSONIC FLIGHT SYSTEMS

Award Year / Program / Phase: 1990 / SBIR / Phase II
Agency / Branch: DOD / USAF
Principal Investigator: Henry L Moody
Award Amount: $70,000.00
Abstract:
Engine inlets for hypersonic vehicles are critical technology areas because of the possible occurance of shockwave impingement, the need for sharp leading edge radii and the requirement of multimission use. this study proposes the design and development of an engine inlet leading edge concept that… More

LIGHTWEIGHT COOLING COMPONENT DEVELOPMENT

Award Year / Program / Phase: 1990 / SBIR / Phase I
Agency / Branch: DOD / NAVY
Principal Investigator: Liam S Groener
Award Amount: $50,126.00
Abstract:
The objective of the proposed innovation is to improve the thermal performance and reduce the weight of heat exchangers used in military combat vehicles. this objective shall be accomplished by using technology that atss has developed and applied in the design and fabrication of compact-actively… More

LASER BRAZING CERAMICS TO METALS

Award Year / Program / Phase: 1990 / SBIR / Phase I
Agency / Branch: DOD / NAVY
Principal Investigator: David G Paquette
Award Amount: $55,282.00
Abstract:
A methodology for joining rf or ir dome materials to metals by laser brazing will be developed and demonstrated. the approach used will avoid thermal stress cracking of the ceramic during brazing by minimizing the mass of material that must be heated to brazing temperature. brazing experiment… More

HIGH TEMPERATURE RAKE PROBE FOR ARC-JET TESTS

Award Year / Program / Phase: 1990 / SBIR / Phase I
Agency / Branch: DOD / USAF
Principal Investigator: Henry L Moody
Award Amount: $50,787.00

LASER BRAZING CERAMICS TO METALS

Award Year / Program / Phase: 1991 / SBIR / Phase I
Agency / Branch: DOD / NAVY
Principal Investigator: Liam S Groener , Principal Investigator
Award Amount: $49,671.00

HIGH TEMPERATURE RAKE PROBE FOR ARC-JET TESTS

Award Year / Program / Phase: 1992 / SBIR / Phase II
Agency / Branch: DOD / USAF
Principal Investigator: Henry L Moody
Award Amount: $493,928.00
Abstract:
The objective of the program is to design rake probes that can accurately measure and map arc-jet exist plane flow quantities. three rake probes shall be designed that can map out the aerodynamic properties of the test section in high-enthalpy/highpressure arc-jets. the first probe shall be a… More

ADVANCED THERMAL PROTECTION MATERIALS TEST CONFIGURATION

Award Year / Program / Phase: 1992 / SBIR / Phase I
Agency / Branch: DOD / USAF
Principal Investigator: Liam S. Groener
Award Amount: $48,764.00
Abstract:
The specifications and preliminary hardware designs for a new test configuration for the aedc heat facility will be developed. this test configuration is tailored specifically for the evaluation of thermal protection materials for hypersonic aerodynamic weapons (haws). in particular, it will provide… More

LASER BRAZING CERAMICS TO METALS

Award Year / Program / Phase: 1994 / SBIR / Phase II
Agency / Branch: DOD / NAVY
Principal Investigator: Liam S Groener , Principal Investigator
Award Amount: $450,000.00
Abstract:
The cooling systems used with the diesel engines of unmanned aerialvehicles (uavs) consists of a large liquid-to-air heat exchanger. this heat exchanger requires a large frontal area, which can lead to packaging problems and an increase in the uav-s aerodynamic drag. atss has developed a technology… More