Experimental Analysis of the Helicon Injected Inertial Plasma Electrostatic Rocket (HIIPER)

Author:

Ahern Drew M.1,Miley George H.1,Al-Rashdan Hussein1,Altun Oguzhan1,Berland Grant1,Broemmelsiek Emil1,Chen Zhengyu1,Dong Zongxu1,Thirumalaisamy Mruthun1,Valiaveedu Albert1

Affiliation:

1. University of Illinois, Urbana-Champaign

Publisher

American Institute of Aeronautics and Astronautics

Reference36 articles.

1. Initial Performance Evaluation of a Gridded Radio Frequency Ion Thruster

2. Ulmen, B. "Formation and Extraction of a Dense Plasma Jet from a Helicon-Plasma-Injected Inertial Electrostatic Confinement Device," Ph.D. Dissertation, Nuclear,Plasma, and Radiological Engineering Dept.University of Illinoisat Urbana-Champaign, Champaign, IL,2013.

3. Ahern, D. "Investigation of a Space Propulsion Concept Using Inertial Electrostatic Confinement," Ph.D. Dissertation,Dept. of Aerospace Engineering, Universityof Illinois at Urbana-Champaign, Champaign, IL,2018.

4. Experimental Studies of the Helicon Injected Inertial Plasma Electrostatic Rocket (HIIPER)

5. Plasma ionization by helicon waves

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