Development and testing of advanced shaped charge meteoritic simulators. Part I - Shaped charge design and development
Meteoritic simulators using conical-shaped or hyperbolic-shaped charges that explosively propel metal jets
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Meteoritic simulators using conical-shaped or hyperbolic-shaped charges that explosively propel metal jets
Application plan for tasks to be accomplished on board Manned Orbital Research Laboratory
Conical bearing transducer suitable for gimbal axis support of gyro
Four electrode impedance plethysmographic system for measuring left ventricular output
Design, fabrication, and testing of integral lubrication pump for hypergolic turboalternator power system
Design criteria documents for aerospace equipment for functioning under various environmental conditions, discussing environment selection, statistical data use and methods
Ultrapure copper fluoride synthesis, analytical techniques, and production of one kilogram for cathode material
Operational performance of squeeze-film bearing with incorporated piezoelectric driver gyro
Multiple-mission telemetry system operations with Mariner Mars 69 and Pioneers, and clock synchronization equipment
Modifications to design of electronic controlled commutator of brushless dc torque motor
Static tests to determine effects of throat inlet concepts on forward-radiated fan noise of 707-320B/C airplanes
The author has identified the following significant results. Comparison between ERTS-1 image scale 1:1,000,000 and CETENAL's charts scale 1:50,000 in irrigated land surface determination in one selected spot gave the following results: Surface on CETENAL's charts 129,900 Has. and arbitrarily we gave 100 percent to this value. Surface on image 122,400 Has., 94.5 percent of the first value. It is necessary to use all four bands to have optimum results on the interpretation. The Principal investigator made use of photointerpretation techniques only, mostly monoscopically.
Several versions of the 100K bit chip, which is configured as a single serial loop, were designed, fabricated and evaluated. Design and process modifications were introduced into each succeeding version to increase device performance and yield. At an intrinsic field rate of 150 KHz the final design operates from -10 C to +60 C with typical bias margins of 12 and 8 percent, respectively, for continuous operation. Asynchronous operation with first bit detection on start-up produces essentially the same margins over the temperature range. Cost projections made from fabrication yield runs on the 100K bit devices indicate that the memory element cost will be less than 10 millicents/bit in volume production.
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The three components required to modify the furnace for batch and continuous recharging with granular silicon were designed. The feasibility of extended growth cycles up to 40 hours long was demonstrated by a recharge simulation experiment; a 6 inch diameter crystal was pulled from a 20 kg charge, remelted, and pulled again for a total of four growth cycles, 59-1/8 inch of body length, and approximately 65 kg of calculated mass.
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Significant progress is reported in fabricating a 4 sq cm cell having a 10.1 percent conversion efficiency and a 10 sq cm cell having a 9.2 percent conversion efficiency. The continuous (SCIM) coater succeeded in producing a 16 sq cm coating exhibiting unidirectional solidification and large grain size. A layer was grown at 0.2 cm/sec in the experimental coater which was partially dendritic but also contained a large smooth area approximately 100 micron m thick. The dark characteristic measurements of a typical SCC solar cell yield shunt resistance values of 10K ohms and series resistance values and 0.4 ohm. The production dip-coater is operating at over 50 percent yield in terms of good cell quality material. The most recent run yielded 13 good substrates out of 15.