Small satellite missions requiring attitude control can realize significant mass savings by extending the moment arm of a propulsion-based system. Replacing traditional torque rods and reaction wheels with small thrusters on extendable booms can significantly reduce the mass of the ACS. Small satellite buses pose significant integration challenges when incorporating electric micro-thrusters. Generally these satellites have low power capability and small geometries. This impacts attitude determination and control system (ADACS) thruster performance significantly, as it results in low thrust capability (due to power limitations) and small torque moment arms (due to size limitations). To address these technical challenges, the Air Force Resear...
To make the most of ridesharing opportunities, small satellite (SmallSat) mission designers endeavor...
Spacecraft, intended for solar sailing mission rely on deployable systems to achieve large area to m...
Thesis (Ph.D.)--University of Washington, 2020CubeSats and other small satellites in the 3-25 kg ran...
Abstract. Small satellite missions requiring attitude control can realize significant mass savings b...
Rationale for the inclusion of deployable structures onboard small satellites is ever increasing. Fo...
Composite booms are often adopted onboard spacecraft to modify inertia properties and/or to move ins...
Since the beginning of space history new innovative ideas have been driving space scientists to deve...
Pulsed Plasma Thrusters (PPTs) are finding renewed user appeal due to the growth in small satellite ...
This work presents the first known energy storage and attitude control subsystem (ESACS) for small s...
This work presents the first known energy storage and attitude control subsystem (ESACS) for small s...
Electric propulsion (EP) project focused on designing, constructing, testing, and ultimately optimiz...
This electric propulsion (EP) project is focused on designing, constructing, testing, and optimizing...
This thesis deals with the further development of a boom deployment mechanism with integrated boom r...
Low thrust electric propulsion systems find a promising application field on small-to-medium sized s...
A recently emerged driving requirement for microsatellites is a precise and fast attitude maneuverin...
To make the most of ridesharing opportunities, small satellite (SmallSat) mission designers endeavor...
Spacecraft, intended for solar sailing mission rely on deployable systems to achieve large area to m...
Thesis (Ph.D.)--University of Washington, 2020CubeSats and other small satellites in the 3-25 kg ran...
Abstract. Small satellite missions requiring attitude control can realize significant mass savings b...
Rationale for the inclusion of deployable structures onboard small satellites is ever increasing. Fo...
Composite booms are often adopted onboard spacecraft to modify inertia properties and/or to move ins...
Since the beginning of space history new innovative ideas have been driving space scientists to deve...
Pulsed Plasma Thrusters (PPTs) are finding renewed user appeal due to the growth in small satellite ...
This work presents the first known energy storage and attitude control subsystem (ESACS) for small s...
This work presents the first known energy storage and attitude control subsystem (ESACS) for small s...
Electric propulsion (EP) project focused on designing, constructing, testing, and ultimately optimiz...
This electric propulsion (EP) project is focused on designing, constructing, testing, and optimizing...
This thesis deals with the further development of a boom deployment mechanism with integrated boom r...
Low thrust electric propulsion systems find a promising application field on small-to-medium sized s...
A recently emerged driving requirement for microsatellites is a precise and fast attitude maneuverin...
To make the most of ridesharing opportunities, small satellite (SmallSat) mission designers endeavor...
Spacecraft, intended for solar sailing mission rely on deployable systems to achieve large area to m...
Thesis (Ph.D.)--University of Washington, 2020CubeSats and other small satellites in the 3-25 kg ran...