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Satelite Propulsion Component Developments - Design and Qualification of an Improved Latch Valve

The original Ball Latch Valve was developed between 2004 and 2007, based on a Swagelok design, and between 2008 an

Germany

GT17-117MP

OMNIDEA-RTG GMBH
Magnetic Powder as Propellant in Electrostatic Thrusters (MPEP)

The main objectives of this project were to develop a thruster prototype based on magnetic powder electrostatic propulsion and to test it in vacuum with direct thrust measurements. The aim was to check the robustness of the concept and to measure and calculate important performance parameters such as thrust and specific impulse, to allow a comparison with other thruster technologies. This project demonstrated for the first time the feasibility of electrostatic propulsion based on powder emission.

Austria

S 2020-02-a

FOTEC GmbH
Consolidation of mN-FEEP Thruster Performance (mN-FEEP 4)

The first steps have been taken to establish a non-explosive, harmless Indium-based 100W electric propulsion system for small and medium satellites. The activity successfully developed a breadboard that included all necessary functions for controlling a micro thruster, including temperature sensing and control, generation of the high voltage supplies for the ion emitter and extractor as well as heating and bias voltage supply for the charge balancing.

Austria

T119-402MP

FOTEC Forschungs- und...

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