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Efficient De-Orbiting of Micro- and Nano Satellites using the IFM Nano Thruster

Alexander Reissner1,Bernhard Seifert1,Nembo Buldrini1,David Jelem1,Richard Sypniewski2
FOTEC1Fotec2

Document details

Publishing year2017 PublisherESA Space Debris Office Publishing typeConference Name of conference7th European Conference on Space Debris
Pagesn/a Volume
7
Issue
1
Editors
T. Flohrer, F. Schmitz

Abstract

FOTEC is currently commercializing the IFM Nano Thruster through its Spin-Off Company AMR Propulsion Innovations. Building on the extensive development history of FOTEC in the frame of ESA Science programs, this new product provides an improvement of about a factor of 5 in the total impulse density with respect to other electric propulsion systems. This makes it particularly suitable for active de-orbiting. The paper will present teh technolgoy, but also test results from the acceptance testing of a flight model that will be delivered to a commercial customer early 2017. Also, several de-orbiting scenarios using this thruster will be presented.

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