TDO0157 PUB Prototech fuel cell - esa-tec.eu · • Distributed.renewable.energy.systems. •...
Transcript of TDO0157 PUB Prototech fuel cell - esa-tec.eu · • Distributed.renewable.energy.systems. •...
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Low mass, compact Regenerative Fuel Cell System (RFCS)
Category: Energy Reference: TDO0157 Broker Company Name: Prekubator TTO Broker Name: Fredrik Fjellså Telephone: +47 51 87 40 26 Email: [email protected]
Abstract The RFCS technology is developed for use on large telecom satellites as a low mass alternative to batteries. The technology can be utilized in a wide range of energy storage systems where mass is a critical factor, and especially where discharge times are larger than 1 hour.
Description The Regenerative Fuel Cell System (RFCS) uses hydrogen and oxygen to generate power in an electrochemical reaction within a fuel cell, producing electricity and water. The water is converted back to hydrogen and electricity in an electrolyser. The hydrogen can be stored in a pressure tank or in metal hydride with integrated heat storage. The fuel cell, electrolyser and the gas storage system are the main components and the heaviest parts in a RFCS system. The development activities have focused on mass reduction of these components as well as safety and operational aspects. The technology has been tested in a closed loop system, and operated autonomously for 1350 cycles, equivalent to a 15-‐year lifetime of a GEO satellite. The technology can be adapted to different sizes, from a few hundred watts to hundreds of kilowatts.
Innovations and advantages of the offer The technology offers high specific energy and power density:
• Fuel cell power > 1kW/kg • Electrolyser power >1kW/kg • Electrolyser output pressure: 100 bar • Energy density 250 – 600 Whr/kg (depending on discharge/charge time) • Integrated heat storage
Application Typical applications could be:
• Autonomous measurement platforms • Autonomous communication stations
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• Aircraft systems • Back-‐up systems for remote areas • Distributed renewable energy systems • Drones and remotely operated aircrafts (Fuel Cell and Storage only)
Description of Space Heritage The technology was originally developed for energy storage for large telecom satellites. Next-‐generation telecom satellites will demand increasing amounts of power up to 30 kW or more. Battery technology able to sustain 30kW over an eclipse length of 72 minutes would have a major impact on the total mass of the satellite. Thus alternative technologies such as the RFCS are attractive, and ESA has funded a series of projects related to the development of a RFCS for telecoms satellites.
This Technology Description was downloaded from www.esa-‐tec.eu
High Temperature Proton Exchange Membrane (HT-‐PEM) fuel cell stack used in testing the closed-‐loop RFCS breadboard demonstrator.