Temperature-Dependent Performance of Electrospray Thrusters with ASCENT Monopropellant
In this work, we investigate the emission characteristics and performance of a passivelyfed
electrospray thruster with ASCENT (AF-M315E) monopropellant at temperatures from 20C to …
electrospray thruster with ASCENT (AF-M315E) monopropellant at temperatures from 20C to …
Adaptive and Responsive Design Under Uncertainty for Resource-Constrained Small Satellites
MG Fifield - 2023 - dspace.mit.edu
The space environment that satellites face is uncertain and challenging for survival and
operation. Traditionally, satellite design methods mitigate the effects of uncertainty through …
operation. Traditionally, satellite design methods mitigate the effects of uncertainty through …
Performance Characterization of High-Density Electrospray Thrusters
MN Corrado, C Wangari, MR Finch, L Parameswaran… - 2024 - dspace.mit.edu
Research and development into electrospray propulsion technology has accelerated in
recent decades. The state of the art in electrospray propulsion is microfabricated …
recent decades. The state of the art in electrospray propulsion is microfabricated …