This work reports a novel design and batch fabrication method of an electrospray emitter suitable for space propulsion. Our device only involves two-step photolithography and electroplating processes, in sharp contrast to traditional SiO2/based out-of-plane design and labor-intensive fabrication process. In-plane metallic emitter nozzles with 100 times longer effective nozzle length were fabricated consistently with high aspect ratio post arrays embedded within the nozzle as a flow homogenizer. The novelty of this work lies in that this integrated thruster/actuator provides a compact, reliable propulsion subsystem with the feasibility of thrust vectoring
The micro-newton thrust generated by an ionic liquid electrospray thruster (ILET) can be used for dr...
Thesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 201...
Microfabrication, wafer-level integration, and characterization of internally fed arrays of electros...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Electrical Engineering and Computer...
Microfabricated electrospray thrusters could revolutionize the spacecraft industry by providing effi...
A low power porous electrospray thruster propulsion system is being developed and tested by a consor...
A UK-Austrian consortium led by AVS UK in collaboration with the University of Southampton (UoS) and...
Micro-electrospray thrusters are a high-performancepropulsion option for nanosatellites, achieving a...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2004....
Electrospray thrusters can deliver the efficient primary propulsion and attitude control actuation n...
Microfabricated electrospray thrusters are widely acknowledged as one of the most promising technolo...
Electrospray thrusters utilize a strong electric field to extract and accelerate charged particles c...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2008.In...
Miniaturized electrical thrusters based on electrospray (or colloid) emitters could rev-olutionize t...
Electric propulsion is becoming an increasingly desirable technology as space missions become more c...
The micro-newton thrust generated by an ionic liquid electrospray thruster (ILET) can be used for dr...
Thesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 201...
Microfabrication, wafer-level integration, and characterization of internally fed arrays of electros...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Electrical Engineering and Computer...
Microfabricated electrospray thrusters could revolutionize the spacecraft industry by providing effi...
A low power porous electrospray thruster propulsion system is being developed and tested by a consor...
A UK-Austrian consortium led by AVS UK in collaboration with the University of Southampton (UoS) and...
Micro-electrospray thrusters are a high-performancepropulsion option for nanosatellites, achieving a...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2004....
Electrospray thrusters can deliver the efficient primary propulsion and attitude control actuation n...
Microfabricated electrospray thrusters are widely acknowledged as one of the most promising technolo...
Electrospray thrusters utilize a strong electric field to extract and accelerate charged particles c...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2008.In...
Miniaturized electrical thrusters based on electrospray (or colloid) emitters could rev-olutionize t...
Electric propulsion is becoming an increasingly desirable technology as space missions become more c...
The micro-newton thrust generated by an ionic liquid electrospray thruster (ILET) can be used for dr...
Thesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 201...
Microfabrication, wafer-level integration, and characterization of internally fed arrays of electros...