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The main objective of the intelligent COTS-based Power Stages (iCOTS) project consisted of the following aspects:
- Design and implementation of a BLDC power stage for robotic space application
- A modular design for the evaluation of power electronics in robotic space application based on COTS GaN-FETs
- Definition of the design process and the appropriate selection of COTS components
- Radiation test of selected COTS components
DFKI - Deutsches...
The goal of the Powersail project is to demonstrate the potential of amorphous silicon (a-Si) deposited on ultralight space-grade polyimide for solar power satellites (SPS). State of the art solutions are III-V compound semiconductor triple junction-based PV modules, which are 100 times too expensive and one order of magnitude too heavy to build a competitive SPS with terrestrial microwave energy collection infrastructure.
CSEM SA. Centre Suisse...
The main objective of the study is to investigate the technological feasibility of implementing the GE⊕-LPS concept, and its role as a prototype for proposed cislunar scenarios supplying electric power to Earth. The methodological approach to the study has been to identify and validate the most simple and effective solutions which ould be practically implemented with known and existing technologies and approaches.
Astrostrom GmbH
The activity investigated a novel hybrid magnetic shielding system that uses both passive and active cancelation. The design and simulations used, along with the characterisation and measurements taken on the optimised system, are summarised in the executive summary report, and described in more detail in the Final Report. This activity was divided in two main work packages: study of optimisation and magnetic shield prototype.
RAL (Rutherford Appleton...
Xerotech Ltd
To develop large-scale infrastructure on the Moon, many different systems will have to be shipped to the Moon to produce the necessary components. This means that the traditional design of systems cannot be assumed and a production machine cannot be expected to provide its own power especially when power demand is in the 100 kW – 1 MW range.
MAANA Electric
Radioisotope generators provide electrical power for spacecraft by converting the energy released by the decay of radioisotope fuel into electricity. Non-thermal converters (voltaic devices) make use of the photoelectric effect much in the same way a solar cell does. They are much easier to miniaturise for future chip-sized deep space probes, however performance quickly degrades due to radiation damage.
Progetti e Campioni Srls
Space Based Solar Power concepts promise the generation of large amounts of renewable power by launching vast Solar Power Satellites (SPS) into space and beaming the power back to rectennas on Earth. Due to diffraction physics, large scale arrays delivering 2GW of power to the ground will be on the order of a kilometre in length and have masses between 2,000 and 10,000 tonnes. As of January 2020, the amount of debris orbiting the Earth exceeded 8,000 metric tonnes.
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