Development of cathodic electrocatalysts for use in low temperature H2/O2 fuel cells with an alkaline electrolyte, January 1-31, 1966
Cathodic electrocatalyst development for use in low temperature hydrox fuel cell in alkaline electrolyte
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Cathodic electrocatalyst development for use in low temperature hydrox fuel cell in alkaline electrolyte
Performance prediction on primary hydrogen oxygen fuel cells for spacecraft power supplies
Transient temperature and voltage response characteristics of fuel cell system predicted by thermodynamic model
Results of experiments on hydrogen-oxygen fuel cells show that higher current densities are obtained with cell anodes having a 100 micron thin active layer of porous nickel containing silver electrocatalyst. Increase in current density is attributed to a convective mass transport mechanism.
High performance light weight electrodes for hydrogen oxygen fuel cells
Simulated hydrogen leakage in electrolytic hydrogen-oxygen fuel cells
Fuel cell electrolyte properties - solubility of hydrogen and oxygen in KOH and LiOH, diffusivity of oxygen and hydrogen in KOH, and density and vapor pressure of KOH and LiOH
Fuel cell uses a porous cathode through which is fed a solution of iodine in aqueous iodide solution, the anode is a hydrogen electrode. No activation polarization appears on the cathode because of the high exchange-current density of the iodine-iodide electrode.
Fuel cell studies on reversibility of organic reactions, oxygen dissolution reaction, and organic adsorption on zinc electrodes of silver zinc batteries
The PC8B-4 fuel cell electrical power supply is an electrical powerplant designed to convert the chemical reaction of hydrogen and oxygen into electrical energy. It utilizes catalyzed electrodes with a potassium hydroxide electrolyte. The powerplant and test stand control unit are described together with a specifications summary. Separate sections deal with: performance, reactants supply and control, heat removal, water removal instrumentation, operation, and safety considerations.
The development and characteristics of advanced spacecraft fuel cell systems are discussed. The system is designed to operate on low pressure, propulsion grade hydrogen and oxygen. The specific goals are 10,000 hours of operation with refurbishment, 20 pounds per kilowatt at a sustained power of 7 KW, and 21 KW peaking capability for durations of two hours. The system rejects waste heat to the spacecraft cooling system at power levels up to 7 KW. At higher powers, the system automatically transfers to open cycle operation with overboard steam venting.
High power-density, self-regulating fuel cell develops electrical power from catalyzed reaction between methanol and atmospheric oxygen. Cells such as these are of particular interest, because they may one day offer an emission-free, extremely efficient alternative to internal-combustion engines as power source.
The main objectives of the SOFC (solid oxide fuel cell) project are to (1) identify viable and cost-effective techniques to prepare cell components for stable MSOFCs (monolithic SOFCs); (2) fabricate half and single cells; and (3) evaluate their performances. The approach used to fabricate stable MSOFCs is as follows: (1) the electrolyte layer is prepared in the form of a honeycomb structure by alloy oxidation and other cell components are deposited on it; (2) the electrolyte and anode layers are deposited on the cathode layer, which has a porous, honeycomb structure; and (3) the electrolyte and cathode layers are deposited on the anode layer. The current status of the project is reported.
The development of thin-film solid oxide fuel cells (TFSOFCs) and a method of fabricating them have progressed to the prototype stage. This can result in the reduction of mass, volume, and the cost of materials for a given power level.
Chemistry of fuel cell reactions - Potentials of zero charge, electrocatalysis, electrode reactions, model porous electrode, potential sweep, and proton transfer across double layers
Design and development of the ion-exchange membrane fuel cell intended to furnish electric power and drinking water to the gemini spacecraft
Fuel cell systems using storable propellants as primary or secondary reactants
Gaseous electrolytes and electrode behavior at elevated temperatures evaluated for battery and fuel cell application