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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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Improved Stability of Double Base Propellants
Amount: $1,466,078.00This Phase II.5 project is focused upon the final determination of a DB propellant formulation for propulsive units on the NACES ejection seat, which meets service life requirements under extreme temp ...
SBIRPhase II2017Department of Defense Navy -
Miniature Extendable Nozzles or Actuating Nozzles for Improved ISP of Divert and Attitude Control System (DACS) Thrusters
Amount: $971,633.00Analytical Services, Inc., is pleased to present this proposal for a lightweight, low cost, high area ratio extendible nozzle design that will provide significant increases in solid divert and attitud ...
SBIRPhase II2014Department of Defense Missile Defense Agency -
Low-Cost Manufacturing Technique for Advanced Regenerative Cooling for In-Space Cryogenic Engines
Amount: $750,000.00The goal of the proposed effort is to use selective laser melting (SLM, an additive manufacturing technique) to manufacture a hot fire-capable, water-cooled spool piece that features an advanced regen ...
SBIRPhase II2014National Aeronautics and Space Administration -
Miniature Extendable Nozzles or actuating nozzles for improved ISP of DACS thrusters
Amount: $149,964.00ASI is pleased to team with ATK to present a novel concept for enabling large nozzle area ratio increases for future solid divert and attitude control system (SDACS) valves/thrusters. The proposed ef ...
SBIRPhase I2013Department of Defense Missile Defense Agency -
Low-Cost Manufacturing Technique for Advanced Regenerative Cooling for In-Space Cryogenic Engines
Amount: $124,436.00The goal of the proposed effort is to demonstrate feasibility of using selective laser melting (SLM, an emerging manufacturing technique) to manufacture a subscale combustion chamber liner that featur ...
SBIRPhase I2013National Aeronautics and Space Administration -
Solid Rocket Motor for Ultralow Temperature Operation During the Mars Sample Return Mission
Amount: $124,868.00A small Mars (or other celestial body) ascent vehicle is unlikely to achieve the necessary propellant fraction required to achieve orbit. Scaling down of liquid propulsion systems, as shown in the fi ...
SBIRPhase I2013National Aeronautics and Space Administration -
Low Cost Refractory Matrix Composite Thruster for Mars Ascent Vehicles
Amount: $124,990.00The long-term goal for this effort is to develop a low-cost, high-temperature thruster. Within the attitude control propulsion community, many efforts have focused on development of ultra-high temper ...
SBIRPhase I2012National Aeronautics and Space Administration -
Confined Submerged Jet Enhancement of Regenerative Cooling Heat Transfer Coefficients in Liquid Rocket Engines
Amount: $149,910.00ABSTRACT: In the proposed effort, ASI will demonstrate the feasibility of a practical, proven method for significantly increasing the heat transfer coefficient inside regenerative cooling channels. ...
SBIRPhase I2012Department of Defense Air Force -
Low Power, Low Cost Igniter for Nonhypergolic Mars Ascent Vehicle
Amount: $99,995.00Decomposing monopropellant hydrazine across a spontaneous catalyst bed is the gold standard for small propulsion systems responsible for attitude control on satellites and spacecraft. Such a propulsi ...
SBIRPhase I2011National Aeronautics and Space Administration -
Radiation Hardening Manufacturing Technology
Amount: $99,984.00BMDS components must function reliably when exposed to radiation, including both nuclear weapon and natural space environments. Current tools will not allow correct evaluations of system performance. ...
SBIRPhase I2011Department of Defense Missile Defense Agency
