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Analytical Services, Inc.
UEI: K5Y3MDHD2MB5
# of Employees: 145
HUBZone Owned: No
Socially and Economically Disadvantaged: Yes
Woman Owned: No
Award Charts
Award Listing
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Qu Tubes for High Temperature Heat Rejection
Amount: $699,128.00ABSTRACT: In our proposed Phase II effort, we will be demonstrating long-lived aqueous aluminum heat pipes. The work will directly demonstrate the corrosion inhibition character of two different aqu ...
SBIRPhase II2011Department of Defense Air Force -
ASSIST: Predicting Flaw Initiation and Propagation in Aged Solid Rocket Motors
Amount: $749,184.00ABSTRACT: When a solid rocket motor propellant grain contains one or more flaws (cracks, debonds, casting voids) or develops them as it ages, the risks of testing that motor is significantly increase ...
SBIRPhase II2011Department of Defense Air Force -
Improved Stability of Double Base Propellants
Amount: $999,951.00In the proposed effort, ASI will be teaming with a major propulsion contractor to develop next generation thermal stabilizers for double base propellants. The scope includes chemical synthesis, propel ...
SBIRPhase II2011Department of Defense Navy -
Constant Pressure Aerospike for Interceptor Axial Propulsion
Amount: $99,982.00Our proposed effort will be used to determine the feasibility of a deeply-throttleable aerospike engine that maintains constant specific impulse performance, regardless of the throttle setting. The d ...
SBIRPhase I2010Department of Defense Missile Defense Agency -
Qu Tubes for High Temperature Heat Rejection
Amount: $99,992.00In our proposed effort, we intend to perform high temperature (100-200 Deg C) characterization of an ultra-advanced heat pipe to determine feasibility of using it in high temperature space radiators. ...
SBIRPhase I2010Department of Defense Air Force -
Test Methodology and Equipment for Radiation Hardened Interceptors
Amount: $999,974.00The Radiation Test Environment Simulation Toolkit (RadTEST) is capable of flowing down radiation environment requirements to the development of test plans, post-test analysis, and test reports. It''s ...
SBIRPhase II2010Department of Defense Missile Defense Agency -
Ultralightweight, Regeneratively Cooled Combustion Chamber for Mars Ascent Vehicles
Amount: $99,999.00We propose a high-pressure, regeneratively-cooled combustion chamber that uses novel material selection for extreme reductions in mass. These materials are manufactured using proven processes, proces ...
SBIRPhase I2009National Aeronautics and Space Administration -
Advanced Ionic Liquid Monopropellant for Payload Ascent Vehicles
Amount: $99,915.00We propose to develop a monopropellant replacement for hydrazine using eutectic mixtures of ionic liquids (EILs). These liquids offer us the ability to tailor fluid and chemical properties, are safe ...
SBIRPhase I2009National Aeronautics and Space Administration -
Test Methodology and Equipment for Radiation Hardened Interceptors
Amount: $99,964.00ASI, teamed with GH Systems, proposes to integrate the comprehensive material and component database, RadCat™, with 3-D modeling, radiation transport, and electrodynamics software to provide a knowl ...
SBIRPhase I2009Department of Defense Missile Defense Agency -
Improved Stability of Double Base Propellants
Amount: $149,809.00ASI is proposing a novel double base stabilizer concept that capitalizes on years of environmental research, including research into the reduction of NOx, SOx, and VOC gases released into the earth''s ...
SBIRPhase I2009Department of Defense Navy
