USE OF A SEALED SILVER-CADMIUM BATTERY ON EXPLORER XII
Performance of a sealed-silver cadmium battery on explorer xii
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Performance of a sealed-silver cadmium battery on explorer xii
Battery charger for Atmosphere Explorer B spacecraft - packaging in aluminum frame rectangular configuration with three separate compartments
High temperature battery development - zeolites, anode and cathode couples, and molten salts
Radiation effects on silver and zinc battery electrodes
X-ray diffraction patterns of nickel-cadmium battery electrodes and stabilization of nickel oxides and hydroxides
Three-day battery capable of operation at temperature of 425 degrees C for use on lunar and planetary probes
Results of a numerical analysis evaluating the feasibility of high-temperature shape memory alloys (HTSMA) for active clearance control actuation in the high-pressure turbine section of a modern turbofan engine has been conducted. The prototype actuator concept considered here consists of parallel HTSMA wires attached to the shroud that is located on the exterior of the turbine case. A transient model of an HTSMA actuator was used to evaluate active clearance control at various operating points in a test bed aircraft engine simulation. For the engine under consideration, each actuator must be designed to counteract loads from 380 to 2000 lbf and displace at least 0.033 in. Design results show that an actuator comprised of 10 wires 2 in. in length is adequate for control at critical engine operating points and still exhibit acceptable failsafe operability and cycle life. A proportional-integral- derivative (PID) controller with integrator windup protection was implemented to control clearance amidst engine transients during a normal mission. Simulation results show that the control system exhibits minimal variability in clearance control performance across the operating envelope. The final actuator design is sufficiently small to fit within the limited space outside the high-pressure turbine case and is shown to consume only small amounts of bleed air to adequately regulate temperature.
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Identification and characterization of battery active compound structures formed on nickel oxide electrode during charging and discharging
Polymer separator materials for heat sterilizable battery
Automatic battery formation cycler and controller to determine charge capacity and to perform charge-discharge operations for electrochemical cells intended for satellite power sources
Radiation effects on silver-zinc battery electrodes
Fabrication and testing of battery separator material of modified polyethylene film
Gamma radiation effects on silver and zinc battery electrodes
Cryptanalytic technique for evaluating nickel- cadmium battery cell failure characteristic data
Develop battery that will meet DS-2 power requirements under specified operational, environmental, and life requirements.
Development of sealed lead-acid battery with lead- calcium grid for space application
Aqueous and nonqueous electrolytic actions, and energy density measurements for dry tape battery