A study of cadmium absorption of resonance neutrons in various foil materials space technology project no. 13
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Feasibility study on accelerating transfer of aerospace technology to commercial industry - aerospace literature applicability to industry
Stress measurements, data acquisition by continuous scanning of strain gauge data, and analysis by computer routine
Conference on aerospace engineering - proposals for auxiliary solar sensors for planetary tracker
Design of advanced Mars exploration spacecraft
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Simulation studies and facilities for atmospheric reentry at hypersonic speeds
Aerospace management technology transfer, discussing conceptual contributions, planning, administrative and evaluation methods
Orbiting STARLAB with laser communication system
Investigation of application of NASA developed technology to cardiovascular and pulmonary patient monitoring to improve availability of data for medical diagnosis
Investigation of techniques to improve performance and service life of nickel-zinc electric batteries for application to low pollutant propulsion systems
Patient monitoring system design and equipment specifications with physiological response display device and warning system
Systems analysis of agricultural and water management information systems utilizing satellite borne multispectral band scanner, radar, and television equipment
Systems analysis and cost estimates of satellite borne remote sensing for wheat crop and fungus disease control and water management
Mathematical models for application of satellite borne multispectral remote sensors to water and wheat production management and wheat fungi control including cost estimates
Aerospace technology direct and derived benefits for public, discussing earth resources program, communication satellites and NASA effect on nonaerospace activities and economy
Nickel-zinc batteries for use in hybrid heat engine/electric systems of low pollutant passenger cars, increasing service life by aerospace technology
Determination of the nature and degree of contamination of mirrors in a vacuum environment in the presence of UV irradiation by outgases from some materials that are candidates for use inside spacecraft and simulated spacecraft environments. A vacuum apparatus was developed for testing contamination of mirrors. Offgases from heated test materials are deposited on a refrigerated mirror, half of which is UV irradiated. Reflectance is measured between 1100 and 25,000 A. Thermofit RNF-100, insulated wire TRT-24-19-V-93, and Eccofoam FS and FPH gave heavier deposits on the nonirradiated mirror. Moxness MS60 SO8, Scotch Tape Y-9050, RTV-577, RTV-41, Stycast 1090, and Epon 934 and 828 gave heavier deposits on the irradiated mirror. Raychem wire 44/0411, polyimide tape X1156, Insulgrease G-640, High Vacuum Silicone Grease, and RTV-602 gave only slight deposits on the irradiated and nonirradiated areas of the mirror.