E3S Web Conf.
Volume 16, 201711th European Space Power Conference
|Number of page(s)||7|
|Section||Power Management & Distribution: High Voltage|
|Published online||23 May 2017|
Development of A Low Cost PPU For Feep Electric Propulsion Using Cots Components
FOTEC Forschungs- und Technologietransfer GmbH
In the frame of the development of an electric-propulsion thruster for Micro- and Nanosatellites, FOTEC has put forward the in-house development of a low cost PPU, capable of driving the thruster with up to 10 kV emitter and -10 kV extractor voltage. After 5 generations of development, the PPU currently used in a thruster testing and qualification campaign has achieved 85% total efficiency including high voltage multiplier stages and protection circuitry. The PPU includes the functionality of the step-up conversion for emitter and extractor, propellant heating and neutralizer-operation within a volume of 90 × 94 × 78 mm, at a weight of less than 230 g and a total cost in production of less than € 1,000. This low cost approach using COTS components is targeting constellations and mega-constellations and is certainly the other extreme compared to the conventional design approach for spacecraft PPUs. In the light of the ongoing discussions of a change in the philosophy of designing spacecraft, going from fail-safe components to a “mass production” strategy which aims for fail-safety by redundancy. This paper also gives a starting point for the discussion on how a possible trade-off between cost and reliability can be achieved.
© The Authors, published by EDP Sciences, 2017
This is an Open Access article distributed under the terms of the Creative Commons Attribution License 4.0, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
Initial download of the metrics may take a while.