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Science and Technology Applications, LLC
http://www.sci-tech-apps.com
UEI: P1EKGM6KQER6
# of Employees: 5
HUBZone Owned: No
Socially and Economically Disadvantaged: No
Woman Owned: Yes
Award Charts
Award Listing
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“Green” Liquid Propellant Upper Stage Engine for Air Launched Targets
Amount: $1,999,990.00Our vision for the next generation missile and space propulsion is a flexible and non-toxic propulsion technology using AF-M315E monopropellant, offering variable thrust with a high degree of mission ...
SBIRPhase II2019Department of Defense Missile Defense Agency -
Low Toxicity, Non-cryogenic Liquid Propellant Upper Stage Engine
Amount: $99,986.00Our vision for the next generation missile and space propulsion engine is a flexible and non-toxic propulsion technology using HAN/kerosene, offering variable thrust with a high degree of mission tail ...
STTRPhase I2019Department of Defense Missile Defense Agency -
Green Liquid Propellant Upper Stage Engine for Air Launched Targets
Amount: $149,897.00Our vision for a "green" upper stage propulsion is a non-toxic multi-use system using HAN and kerosene, offering variable thrust with a high degree of mission tailoring. Additionally, such system will ...
SBIRPhase I2018Department of Defense Missile Defense Agency -
Lowest Lifecycle Cost (LLC) Propulsion System
Amount: $1,499,983.00ABSTRACT:Future military and commercial spacelift systems will utilize reusable systems, consisting of liquid oxygen/hydrocarbon staged combustion engines, in order to increase the military utility by ...
SBIRPhase II2015Department of Defense Air Force -
Lowest Lifecycle Cost (LLC) Expendable Launch Vehicles
Amount: $149,915.00ABSTRACT: To meet the goals of future generation of ELVs, significant improvements must be made in cost. Current expendable launch vehicles are designed using an optimum performance methodology. Rece ...
SBIRPhase I2014Department of Defense Air Force -
High Performance Cooling Methods for Liquid Rocket Engines
Amount: $739,572.00ABSTRACT: To meet the goals for future generation Air Force LOX/Hydrocarbon booster engines, improvements must be made in performance, operability, reusability, reliability, and cost. To date, operat ...
SBIRPhase II2013Department of Defense Air Force -
High Performance Cooling Methods for Liquid Rocket Engines
Amount: $149,974.00ABSTRACT: To meet the goals for future generation Air Force LOX/Hydrocarbon booster engines, improvements must be made in performance, operability, reusability, reliability, and cost. To date, operat ...
SBIRPhase I2012Department of Defense Air Force -
Novel energetic materials from new polyazide ingredients
Amount: $99,979.00Polynitrogen and high-nitrogen compounds hold great potential for High Energy Density Materials (HEDM). Particular advantages of these compounds are their high energy content, environmentally more ben ...
STTRPhase I2009Department of Defense Air Force -
Variable Thrust and Non-Toxic Liquid Propulsion for Mission Flexibility
Amount: $99,995.00Our vision for the next generation missile propulsion is a flexible and non-toxic system using HAN and a storable fuel candidate, offering variable thrust with a high degree of mission tailoring. Addi ...
SBIRPhase I2008Department of Defense Air Force -
Environmentally-Benign Oxidizers for Propulsion
Amount: $749,813.00During Phase II of the proposed program, Science and Technology Applications, LLC (STA), proposes to find a green replacement for ammonium perchlorate (AP). During Phase I of this program, the novel t ...
STTRPhase II2007Department of Defense Air Force
