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Highly miniaturized FEEP propulsion system (NanoFEEP) for attitude and orbit control of CubeSats

  • Published:2018-03 Issue: Volume:144 Page:422-428
  • ISSN:0094-5765
  • Container-title:Acta Astronautica
  • language:en
  • Short-container-title:Acta Astronautica

Author:

Bock Daniel,Tajmar Martin

Funder

Federal Ministry for Economic Affairs and Energy

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference11 articles.

1. Highly miniaturized FEEP thrusters for CubeSat applications;Bock,2014

2. Pico-satellite orbit and attitude control by electric propulsion;Kronhaus;Automatic Control in Aero.,2013

3. "CubeSat Design Specification, Rev. 12," the CubeSat Program;Lee,2009

4. Indium FEEP microthruster experimental charactization;Tajmar;J. Propul. Power,2004

5. NanoFEEP on UWE platform - formation flying of CubeSats using miniaturized field emission electric propulsion thrusters;Bock,2015

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