Add to ORKGThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1997.In...
A thrust stand has been built to measure the force-noise produced by electrostatic micro-Newton (muN...
Deflectable dual beam, linear strip cesium contact, ion thruster system design and performance testi...
A thrust stand for use with high power electric propulsion devices was designed and tested. The thru...
Linear ion thrustor and cesium feed system for possible satellite control systems applicatio
Improvements in electric subsystem and capacity of thrust stand system for testing chemical, sublimi...
Design analyses showed that an ion thruster of approximately 50 cm in diameter will be required to p...
A thrust stand has been designed, built, and tested to measure the roughly 10 mN force produced by a...
This thesis explores the viability of an inverted pendulum-type thrust stand for measuring forces fr...
Development of 8 cm ion thruster technology which was conducted in support of the Ion Auxiliary Prop...
At the Space Engineering (SpE) department of the Delft University of Technology performance testing ...
Miniaturized satellites which are fitted with microthrusters are gaining in popularity over the past...
The arcjet development at the Institute of Space Systems (IRS) at Stuttgart is intended to deorbit s...
College of Engineering; Mechanical and Aerospace Engineering; Advisor: Dr. K. Gabriel Xu; Date: Apri...
System for calibration of load cells and design and development of thrust measuring syste
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1997.In...
A thrust stand has been built to measure the force-noise produced by electrostatic micro-Newton (muN...
Deflectable dual beam, linear strip cesium contact, ion thruster system design and performance testi...
A thrust stand for use with high power electric propulsion devices was designed and tested. The thru...
Linear ion thrustor and cesium feed system for possible satellite control systems applicatio
Improvements in electric subsystem and capacity of thrust stand system for testing chemical, sublimi...
Design analyses showed that an ion thruster of approximately 50 cm in diameter will be required to p...
A thrust stand has been designed, built, and tested to measure the roughly 10 mN force produced by a...
This thesis explores the viability of an inverted pendulum-type thrust stand for measuring forces fr...
Development of 8 cm ion thruster technology which was conducted in support of the Ion Auxiliary Prop...
At the Space Engineering (SpE) department of the Delft University of Technology performance testing ...
Miniaturized satellites which are fitted with microthrusters are gaining in popularity over the past...
The arcjet development at the Institute of Space Systems (IRS) at Stuttgart is intended to deorbit s...
College of Engineering; Mechanical and Aerospace Engineering; Advisor: Dr. K. Gabriel Xu; Date: Apri...
System for calibration of load cells and design and development of thrust measuring syste
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1997.In...
A thrust stand has been built to measure the force-noise produced by electrostatic micro-Newton (muN...
Deflectable dual beam, linear strip cesium contact, ion thruster system design and performance testi...