Microwave device investigations Semiannual progress report, 1 Apr. - 1 Oct. 1969
Summaries of progress in beam plasma interactions, paramagnetic and bulk semiconductor materials, and avalanche diodes
Curtice, W. R.↗
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Infrared spectra of molecules and materials of astrophysical interest Quarterly progress report, 15 jun. - 15 sep. 1970
Infrared spectra of molecules and materials of astrophysical interest Quarterly progress report, 15 Jun. - 15 Sep. 1970
Durig, J. R.↗
On the feasibility of applying pattern recognition concepts for an aircraft approach progress monitor
Pattern recognition concepts applied to synthesis of aircraft approach progress monitor as adjunct to pilot decision process, discussing feasibility experiments
Brand, T. E.↗
Research-Airplane-Committee Report on Conference on the Progress of the X-15 Project
This document is a complication of the papers presented at the Conference on the Progress of the X-15 Project held at the NASA Flight Research Center, Edwards Air Force Base, California, November 20-21, 1961. This conference was held by the Research Airplane Committee of the U.S. Air Force, the U.S. Navy, and the National Aeronautics and Space Administration to report on the technical status of this research airplane. The papers were presented by members of the staffs of North American Aviation, Inc.; Aeronautical Systems Division, U.S. Air Force; Air Force Flight Test Center; and National Aeronautics and Space Administration.
De E Beeler↗
Economic impact of stimulated technological activity. Part 2: Case study, technological progress and commercialization of communications satellites
The economic impact of technological progress in communications satellites is considered, as well as how these impacts affect the firms involved. Influences, if any, on the three major inputs of a nation's economic output (capital, labor, and technology) is discussed.
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A progress report on the development of an augmentor wing jet STOL research aircraft.
The development of the aircraft has progressed to the point where the design of the modifications to the de Havilland C-8A Buffalo is complete and the engines are being tested. The predicted performance shows that the aircraft will be able to take off and land in less than 1500 ft. Simulation studies indicate that the handling qualities of the aircraft, with stability augmentation, will be acceptable for STOL research missions. Special techniques were required, however, for flight path control and transition from cruise to landing configuration .
Quigley, H. C.↗
A progress report - Induction plasma simulation of the GCNR.
Significant progress has been made in the design, construction and operation of induction coupled devices which simulate the open cycle Gas Core Nuclear Rocket. These devices incorporate solid feed of the plasma forming material (uranium and uranium simulating materials), permeable walls, seeding of the propellant, and transpiration cooled, choked flow nozzles. Operating parameters and performance data of devices employing these design features are discussed. A uranium plasma experiment is included. In addition, operating data of several devices which compare theoretical and actual performance at a variety of powers, pressures, frequencies, and sizes are discussed.
Vogel, C. E.↗
Research And Development Contributions to Aviation Progress (RADCAP): Executive summary
Positive contributions of military aeronautical research and development programs to civil aviation are reviewed and some possible future contributions of those military programs are assessed. A summary is presented of detailed results concerned with: (1) review of the progress that has been made in aviation since 1925 and the significant technological advances that have been made; (2) an examination of current and planned military aeronautical research and technology programs and an assessment of their relevancy to the aeronautical R and D needs of civil aviation; (3) the relationship of the development base generated by military programs to the needs of civil airliner design, development, and production; (4) information on aeronautical R and D funding; and (5) the findings and observations of the RADCAP study.
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Ames-aided inertial navigation work - The first two years of progress
A description of work whose broad objective is to attain improved aircraft navigation performance through exploitation of the concept of combining navigation data from several sources in an optimum manner is presented. The system developed as a result of the work, called RAINPAL (Recursive Aided Inertial Navigation for Precision Approach and Landing) is designed to combine precision radio range measurements with data from on-board inertial sensors to achieve precision navigation for approach and landing. The paper describes RAINPAL and the rationale of its design, and also serves as a sort of planning document, including a progress report, a summary of objectives past and present, and an exposition of reasons for doing the work.
Smith, G. L.↗
Use of the Glauber approximation in atomic collisions - A progress report.
Recent progress in the use of the Glauber (1970) theory for estimating atomic collision cross sections is reviewed. It appears that the Glauber approximation is reliable for electron-hydrogen elastic scattering and excitation at incident energies exceeding 30 eV. For more complicated atomic collisions, the usefulness of the Glauber approximation has not yet been significantly tested.
Gerjuoy, E.↗
Progress of the X-15 Research Airplane Program
This compilation consists of papers presented at the fourth conference on progress of the X-15 Research Airplane Program held at the NASA Flight Research Center, Edwards Air Force Base, California, October 7, 1965. This conference was sponsored by the Research Airplane Committee of the U.S. Air Force, the U.S. Navy, and the National Aeronautics and Space Administration. Papers were presented by representatives from the NASA Flight Research Center, the NASA Langley Research Center, the U.S. Air Force Flight Test Center, and the U.S. Air Force Aeronautical Systems Division.
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Canadian ERTS program progress report
Progress of the Canadian ERTS program is provided along with statistics on the production and role of ERTS images both from the CCRS in Ottawa and from the Prince Albert Saskatchewan satellite station. The types of products, difficulties of production and some of the main applications in Canada are discussed.
Morley, L. W.↗
Progress in Aircraft Design Since 1903
The progress of aircraft design technology, described in this booklet in words and pictures, is illustrated in a wall display in the Visitors' Center of the Langley Research Center, National Aeronautics and Space Administration, Hampton, Virginia. The display presents, in miniature but highly detailed and accurate models, a broad panorama of aeronautical development. It begins with the Wright brothers' "Flyer" of 1903 and ends with the current generation of jet transports. In model form, and to a common scale, the aircraft described in this booklet take on added dimension and emphasis. Many of the models in the Langley display were built and contributed by members of the Tidewater Branch of the International Plastic Modelers Society, an international group of scale-model enthusiasts. Certain of the models, for which no commercial kits existed, had to be fabricated completely; that work was done by several talented individuals in the Langley Research Center. A few of the models were donated specifically for the display by the manufacturers of the full-scale aircraft.
David A Anderton↗
Progress of the LASL dry hot rock geothermal energy project
The possibilities and problems of extracting energy from geothermal reservoirs which do not spontaneously yield useful amounts of steam or hot water are discussed. The system for accomplishing this which is being developed first is a pressurized-water circulation loop intended for use in relatively impermeable hot rock. It will consist of two holes connected through the hot rock by a very large hydraulic fracture and connected at the surface through the primary heat exchanger of an energy utilization system. Preliminary experiments in a hole 2576 ft (0.7852 km) deep, extending about 470 ft (143 m) into the Precambrian basement rock underlying the Jemez Plateau of north-central New Mexico, revealed no unexpected difficulties in drilling or hydraulically fracturing such rock at a temperature of approximately 100 C, and demonstrated a permeability low enough so that it appeared probable that pressurized water could be contained by the basement rock. Similar experiments are in progress in a second hole, now 6701 ft (2.043 km) deep, about 1.5 miles (2.4 km) south of the first one.
Smith, M. C.↗
Effect of a progressive sound wave on the profiles of spectral lines. 2: Asymmetry of faint Fraunhofer lines
The absorption coefficient profile was calculated for lines of different chemical elements in a medium with progressive sound waves. Calculations show that (1) the degree and direction of asymmetry depend on the atomic ionization potential and the potential of lower level excitation of the individual line; (2) the degree of asymmetry of a line decreases from the center toward the limb of the solar disc; and (3) turbulent motions 'suppress' the asymmetry.
Kostyk, R. I.↗
Progress in the development of the hollow fiber sodium-sulfur secondary cell
This report describes the development and status of the sodium-sulfur secondary cell which uses fine hollow glass fibers as the electrolyte. Laboratory size cells containing up to 7000 fibers and having capacities up to 5 ampere-hours have been built and operated. These cells have been run at various cycle depths up to 95% of capacity. Lifetime does not depend on depth of discharge up to at least 50% depth and possibly deeper. Rates of charge and discharge of the nominally one hour cells have been varied from three times the design rate to 0.05 times the design rate. Smaller cells operate with essentially no internal resistance increase during their lifetimes of over four months on continuous charge/discharge at the one hour rate. Larger cells assembled with somewhat different mechanical assembly techniques have shorter lives. Two types of failure modes are observed: progressive weakening and breaking of the fibers inside the cell assembly, and fiber breakage at the fiber/tube sheet interface.
Levine, C. A.↗
Conflict and fear over the impacts of science and technology may retard, or may hasten, societal progress
Rapidly changing societal and individual values impact the course of man's future with accompanying conflict, tension and alienation. Conflict and fear over the impacts of science and technology may retard, or may hasten, societal progress. The broadening of the concept of equality of opportunity to an equality of outcome manifests itself by distributing the rewards of society based not on performance but simply on membership in the society. It is concluded that institutional failure caused by organizational and bureaucratic ineffectiveness inhibits change necessary for the solution of societal problems.
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