New Low-Power Plasma Thruster for Nanosatellites

Author:

Sheehan JP,Longmier Benjamin W.,Reese Ingrid,Collard Timothy

Publisher

American Institute of Aeronautics and Astronautics

Cited by 15 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Simulation of the microwave propagation through the plume of a Hall thruster integrated on small spacecraft;Journal of Applied Physics;2022-06-28

2. CI-MBPT line strengths and atomic probabilities for some transitions of neutral iodine;Journal of Physics B: Atomic, Molecular and Optical Physics;2020-06-18

3. Helicon engine in outboard air as a successful solution for maintaining small space vehicle in orbits up to 200 km;XLIII ACADEMIC SPACE CONFERENCE: dedicated to the memory of academician S.P. Korolev and other outstanding Russian scientists – Pioneers of space exploration;2019

4. Experimental Analysis of the Helicon Injected Inertial Plasma Electrostatic Rocket (HIIPER);2018 Joint Propulsion Conference;2018-07-08

5. Simulations and Preliminary Measurements of a Magnetic Nozzle Thrust Vectoring System;2018 AIAA Aerospace Sciences Meeting;2018-01-07

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