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Energy Science Laboratories, Inc.
UEI: N/A
# of Employees: 12
HUBZone Owned: No
Socially and Economically Disadvantaged: No
Woman Owned: No
Award Charts
Award Listing
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Carbon Brush Heat Exchanger
Amount: $500,000.00N/A
SBIRPhase II1994National Aeronautics and Space Administration -
FIBER ELECTROFLOCKING
Amount: $65,000.00N/A
SBIRPhase I1994National Science Foundation -
A THERMAL COMPOSITE PLASMA FACING MATERIAL
Amount: $500,000.00MATERIALS EROSION IN THE HIGH TEMPERATURE RADIATIVE ENVIRONMENT OF THERMONUCLEAR REACTORS SEVERELY LIMITS DESIGN OPTIONS. LOWER SURFACE TEMPERATURES AND REDUCED EROSION OF OF THE PLASMA FACING MATERIA ...
SBIRPhase II1993Department of Energy -
High Emissivity Arcjet Anode
Amount: $74,969.00Improved cooling of the anode can increase the efficiency and lifetime of arcjet thrusters. Smooth tungsten anodes have low emissivity ~0.3 that severely limits radiative cooling heat transfer can be ...
SBIRPhase I1993Department of Defense Air Force -
Z-FIBER REINFORCEMENT OF LAMINATED COMPOSITIES
Amount: $75,000.00N/A
SBIRPhase I1993Department of Defense Air Force -
Flocked Carbon Heat Exchanger Tubing
Amount: $100,000.00N/A
SBIRPhase I1993Department of Defense Air Force -
Carbon Brush Heat Exchanger
Amount: $50,000.00N/A
SBIRPhase I1993National Aeronautics and Space Administration -
LINEAR BOLOMETER ARRAYS FOR INFRARED SPECTROMETERS
Amount: $263,508.00THIS PROJECT WILL DEVELOP LINEAR ARRAYS OF BOLOMETER ELEMENTS FOR USE AS UNCOOLED DETECTORS IN INFRARED SPECTROMETERS. THE ARRAYS WILL INCORPORATE RECENTLY-DEVELOPED THIN FILMS WITH HIGH TEMPERATURE-C ...
SBIRPhase II1992National Science Foundation -
PHASE-CHANGE COMPOSITE THERMAL ENERGY STORAGE FOR NI-H2 BATTERY.
Amount: $64,807.00THERMAL CONTROL IS A DESIGN DRIVER FOR SPACE APPLICATIONS OF NI-H2 BATTERY SYSTEMS. COMPARED WITH THE NI-CD BATTERIES THEY ARE REPLACING, THE NI-H2 BATTERIES REQUIRE LOWER OPERATING TEMPERATURES AND G ...
SBIRPhase I1992Department of Defense Air Force -
Carbon Fiber Thermal Interface Compound
Amount: $63,325.00Interfacial thermal resistance is a major contributor to the temperature gradients existing in satellite systems, causing higher temperatures at the electronic heat sources and larger radiators to pro ...
SBIRPhase I1992Department of Defense Missile Defense Agency