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BUSEK CO., INC.
UEI: SATYSBWG3FL7
# of Employees: 60
HUBZone Owned: No
Socially and Economically Disadvantaged: No
Woman Owned: No
Award Charts
Award Listing
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Qualification of a Satellite on Umbilical Line (SOUL) System for Active Debris Removal (ADR)
Amount: $1,249,762.00Busek Co. Inc has created and patented a tethered spacecraft (s/c) system called SOUL (Satellite on Umbilical Line). Under various sponsorships including the U.S. Air and Space Force, and NASA, five ...
SBIRPhase II2023Department of Defense Air Force -
Flexible Fuel Electron Source for Space Propulsion Systems
Amount: $1,249,708.00Busek and Worcester Polytechnic Institute (WPI) are developing a cathode electron source for spacecraft ion drives that are fueled by a variety of reactive and semi-reactive molecular propellants. The ...
STTRPhase II2023Department of Defense Air Force -
Flexible Fuel Electron Source for Space Propulsion Systems
Amount: $74,979.00Busek and WPI propose to develop a cathode electron source for spacecraft ion drives that are fueled by a variety of reactive and semi-reactive molecular propellants. The cathode may be fueled by ASCE ...
STTRPhase I2023Department of Defense Air Force -
Low Mass High Power Hall Effect Thruster for Enhanced Space Asset Resiliency
Amount: $49,927.00Busek Co. Inc. proposes to develop the world’s best 15 kW Hall Effect Thruster (HET). The thruster will have the lowest mass and highest performance of any HET in its class, including HETs in deve ...
STTRPhase I2022Department of Defense Air Force -
Power Processing Unit (PPU) for 10kW Class Hall Effect Thruster (HET)
Amount: $49,975.00Busek Co. Inc. proposes to develop a cutting-edge 10kW Power Processing Unit (PPU) to enable low-mass, high power, Hall Effect Thruster (HET) systems in the range of 7-20kW. This activity directly sup ...
SBIRPhase I2022Department of Defense Air Force -
Thermal Improvement on 1 Newton ASCENT Thruster Valve Assembly (TVA)
Amount: $149,998.70Busek proposes to develop a novel thermal management system for its 1N ASCENT thruster valve assembly (TVA). Traditionally, monoprop thrusters rely on thermally conductive straps that shunt heat away ...
SBIRPhase I2022Department of Defense Air Force -
Self Tracking Resonant Push-Pull Oscillator With Rectification (STRPOWR) for Faraday Cup Applications[formerly Variable High Voltage DC with 2 KHz AC Modulator for Faraday Cup Applications]
Amount: $749,988.00Advancing the instrumentation to detect elementary particles is critical for future space weather missions. To progress the study of the flow of energy that heats and accelerates solar corona and wind ...
SBIRPhase II2022National Aeronautics and Space Administration -
High Density Plasma Thruster
Amount: $749,976.00In this SBIR program, Busek Co. Inc. is developing a high power, high thrust plasma thruster system for future flight opportunities. The technology works with many propellants including, but not lim ...
SBIRPhase II2022Department of Defense Air Force -
Active Debris Removal System Development
Amount: $249,986.00Busek and its STTR partners are proposing two coupled Orbital Prime proposals addressing all three Tech Tracks identified in the solicitation, culminating with an active debris removal (ADR) demonstra ...
STTRPhase I2022Department of Defense Air Force -
Active Debris Removal System Demonstration
Amount: $249,830.00Busek and its STTR partners are proposing two coupled Orbital Prime proposals addressing all three Tech Tracks identified in the solicitation, culminating with an active debris removal (ADR) demonstra ...
STTRPhase I2022Department of Defense Air Force