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Development of electric and chemical microthrusters
M. Tajmar,
C. A. Scharlemann
Department of Aerospace Engineering
University of Applied Sciences Wiener Neustadt
KAIST
University of Applied Sciences
Research output
:
Contribution to journal
›
Review article
›
peer-review
14
Citations (Scopus)
Overview
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Earth and Planetary Sciences
Electric Propulsion
100%
CubeSat
100%
Indium
50%
Metal Ion
50%
Applied Science
50%
Field Emission
50%
Liquid Rocket Propellant
50%
Microrocket Engine
50%
Liquid Metal
50%
Microsatellite
50%
Physics
CubeSat
100%
Electric Propulsion
100%
Liquid Rocket Propellant
50%
Ion Source
50%
Metal Ion
50%
Applied Science
50%
Field Emission
50%
Liquid Metal
50%
Indium
50%
Engineering
Thruster
100%
Electric Propulsion
33%
CubeSat
33%
Term Stability
16%
Propulsion System
16%
Specific Impulse
16%
Field Emission
16%
Ion Source
16%
Liquid Metal
16%
Material Science
CubeSat
100%
Liquid Metal
50%
Indium
50%