Experimental study of ion thruster operation with oxygen as the propellant
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1983.
Main Author: | Aguilar, Robert Bartoldo |
---|---|
Other Authors: | Manuel Martinez-Sanchez. |
Format: | Thesis |
Language: | eng |
Published: |
Massachusetts Institute of Technology
2012
|
Subjects: | |
Online Access: | http://hdl.handle.net/1721.1/74748 |
Similar Items
-
Prediction of the performance of an ion thruster using Buckminsterfullerene as propellant
by: Torres, Esteban Raul
Published: (2006) -
Studies on the ion-droplet mixed regime in colloid thrusters
by: Lozano-Tovar, Paulo César, 1970-
Published: (2005) -
Silicon wafer integration of ion electrospray thrusters
by: Siegel, Noah Wittel.
Published: (2021) -
Design and manufacture of the next generation of ion electrospray thrusters
by: Freeman, Dakota S.(Dakota Samuel)
Published: (2019) -
Theoretical and experimental investigation of Hall thruster miniaturization
by: Warner, Noah Zachary, 1978-
Published: (2008)