4   Artículos

 
en línea
Anirudh Thuppul, Peter L. Wright, Adam L. Collins, John K. Ziemer and Richard E. Wirz    
Ionic liquid electrospray thrusters are capable of producing microNewton precision thrust at a high thrust?power ratio but have yet to demonstrate lifetimes that are suitable for most missions. Accumulation of propellant on the extractor and accelerator ... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Jared M. Magnusson, Adam L. Collins and Richard E. Wirz    
To better characterize the lifetime and performance of electrospray thrusters, electron emission due to electrode impingement by the propellant cation 1-ethyl-3-methylimidazolium (EMI+) has been evaluated with semi-empirical modeling techniques. Results ... ver más
Revista: Aerospace    Formato: Electrónico

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