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Busek
Analysis of Atmosphere-Breathing Electric Propulsion
Herman IEPC-2019-651 PPE IPS Final
A Breath of Fresh Air: Air-Scooping Electric Propulsion in Very Low Earth Orbit
Theoretical and Experimental Investigation of Hall Thruster Miniaturization by Noah Zachary Warner
BUSEK CO. INC. Modern Spacecraft Performing Interplanetary Missions May Change Velocity by More Than 20,000 Miles Per Hour (32,000 Km/Hr)
Program Management for Concurrent University Satellite Programs, Including Propellant Feed System Design Elements
Busek Propulsion Systems
Propulsion BHT-200-I Thruster
Bi-Sat Observations of the Lunar Atmosphere Above Swirls (Bolas): Tethered Smallsat Investigation of Hydration and Space Weathering Processes at the Moon
Characterization and Anomalous Diffusion Analysis of a 100W Low Power Annular Hall Effect Thruster Megan N
Space Propulsion Technology for Small Spacecraft
Space Technology Mission Directorate
Future Directions for Electric Propulsion Research
Small Satellite Propulsion
The Iodine Satellite (Isat)
Preparation of Papers for AIAA Technical Conferences
Bismuth Vapor Hall Effect Thruster Performance and Plume Experiments
Eight Kilowatt Hall Thruster System Characterization
Top View
Iodine RF Ion Thruster Development Busek Co
High Throughput 600 Watt Hall Effect Thruster for Space Exploration
Innovations in Pulsed Plasma Thrusters to Enable Cubesat Science Missions
Electrospray Propulsion Systems for Small Satellites
An Overview of Cube-Satellite Propulsion Technologies and Trends
Study of RF Plasma Technology Applied to Air-Breathing Electric Propulsion
A Deep Space 6U Cubesat with Mission Enabling Ion Propulsion Technology
The Iodine Satellite (Isat) Project Development Towards Critical Design Review
Busek Electrospray Thrusters Aboard LISA Pathfinder
Lunar and Lagrangian Point L1/L2 Cubesat Communication and Navigation Considerations
Flight Development of Iodine BIT-3 RF Ion Propulsion System for SLS EM-1 Cubesats
State of the Art Small Spacecraft Technology 2018
BUSEK CO. INC. Modern Spacecraft Performing Interplanetary Missions May Change Velocity by More Than 20,000 Miles Per Hour (32,000 Km/Hr)
Overview of Nasa Iodine Hall Thruster Propulsion System Development
Propulsion Survey
Review of Plasma-Induced Hall Thruster Erosion
Overview of Busek Electric Propulsion
Micro RF Ion Engine for Small Satellite Applications
A Compact Low-Power High-Isp Thruster for Microsatellites
Plume Characterization of Busek 600W Hall Thruster Duc Minh Bui
Overview of Iodine Propellant Hall Thruster Development Activities at NASA Glenn Research Center
Design of an Air-Breathing Electric Thruster for Cubesat Applications
Close-Up Survey of Leo Debris Objects
An Exploration of Cubesat Propulsion
Download the Small Spacecraft Technology State of the Art
Breathing Electric Propulsion System
ON-ORBIT SERVICING: INSPECTION, REPAIR, REFUEL, UPGRADE, and ASSEMBLY of SATELLITES in SPACE Joshua P
Overview of Iodine Propellant Hall Thruster Development Activities at NASA Glenn Research Center