Electrical power on-board a space vehicle is arguably one of the key functional requirements of a satellite, enabling the functioning of (scientific) equipment, propulsion and communication. With the steady enhancement of satellite capabilities, these power requirements have increased from around 1W for the Vanguard-1 [link] up to 100's of kW for manned missions. For example, the ISS has a power usage of around 110kW [link] which is generated by multiple solar arrays and balanced with fuel cells and batteries during its 90min orbiting period.
power in space
The majority of spacecraft orbiting the planet use photovoltaic (solar) arrays as their primary source of energy. The great benefit of this technology is that there is no need to bring fuel into orbit which reduces mass and therefore cost. Instead, the solar radiation functions as the 'fuel' with a power density of around 1367 W/m2 at the outer atmosphere [link]. A drawback however is the relatively low energy density and limited lifetime due to the harsh space environment. The use of photovoltaics is actually one of several technologies available to produce power in space. A more complete list can be summarized by:
- Chemical (batteries, turbines)
- Fuel cells
- Cryogenic engines
- Photovoltaics (PV)
- Radioisotope thermal generators (RTG)
- Nuclear dynamic systems (fission, fusion)
The exact choice for any of these systems will depend, among others, on the power level required and the mission duration. In general, short duration flights (e.g. launch systems) often use batteries and/or fuel cells, while long duration missions rely on solar arrays or nuclear systems. For example, the most distant still operating spacecraft, Voyager-1, contains 3 RTG's delivering 157W each (at its current distance of 1.8x1013 m, the incident solar radiation has dropped to below 0.1W/m2). Besides the power generation, two additional elements of the power system are of critical importance, which are the power control/distribution and storage. All three elements are interconnected as supply and demand may be unbalanced requiring a robust distribution networks to control the output over time. In most cases, the source output also changes over time as the fuel is depleted or the generating/conversion efficiency decreases.
The ongoing activities within the Advanced Concept Team span all the above elements by investigating novel methods for generation, distribution and storage of energy in space. By studying new scientific advancements, we aim to provide a first look on future operational capabilities.
Several topics currently under investigation are:
- High energy density materials and devices (aerogels, superconductors and supercapacitors)
- Magnetohydrodynamic (MHD) generators for high power conversion
- Wireless power transfer (earth-orbit, orbit-to-orbit)
For more detailed information on these and related activities you are invited to have a look at the currently ongoing and past projects below.
- Buencuerpo, J., Llorens, J.M., Zilio, P., Raja, W., Cunha, J., Alabastri, A., Zaccaria, R.P., Marti, A., and Versloot, T.W., Light-trapping in photon enhanced thermionic emitters, Optics Express, 23, 2015 (link)
- Versloot, T., Barker, D.J., and Otero One, X., Optimisation of Near-Field Wireless Power Transfer Using Evolutionary Strategies, The 8th European Conference on Antennas and Propagation - EUCAP 14, The Hague, NL, The Hague, Netherlands 2014. (link)
- Summerer, L., Versloot, T., Lecuyot, A., Duvaux-Bechon, I., and Signorini, C., Space and Energy - At the Service of Energy on Earth, IAC-14.C3.1.3, Proceedings 64rd International Astronautical Congress IAC13, Beijing, China 2013. (link)
- Summerer, L., Technical Guidance from the International Safety Framework for Nuclear Power Source Applications in Outer Space for design and development phases, 10th European Space Power Conference - ESPC 14, Noordwijk, NL, Noordwijk, Netherlands 2014. (link)