Theoretical study and engineering development of jimsphere wind sensor final report, 27 feb. 1964 - 1 jun. 1965
Fabrication and flight tests of Jimsphere wind sensor balloons
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Fabrication and flight tests of Jimsphere wind sensor balloons
Development plan for Voyager unmanned Mars orbiter-lander spacecraft - schedules, costs, and problem areas
Jimsphere wind measurement balloon flight test to determine optimum design for flow separation control and wake stabilization
Temperature, ionization level, and electron energy in sparks used for flow velocity measurements
Disrupted vertical laminar downflow effect on microbial burden of hardware subassemblies
Development of magnetic fluid viscous oscillation damper for scientific satellites
Calibration and alignment techniques for inertial sensing unit
One thousand watt continuous wave space environment S band power amplifier development
Theoretical design of spaceborne electrostatically focused klystron amplifier
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Techniques for laboratory calibration and alignment of strapdown inertial sensing unit
Tornado producing thunderstorms using conventional surface and upper air data combined with ATS-III data, discussing mesoscale disturbances and momentum exchange
Design, development, and characteristics of photoheliograph for use with Apollo telescope mount mission
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The engineering feasibility of developing a basic mechanical system necessary for extracting large amounts of power (on the order of 10 to 20 MW) from the wind is considered using the concept of vertical airfoils moving along a closed horizontal track system. Attention is focused on those components necessary for the conversion of wind energy to mechanical energy, although the general characteristics and critical aspects of other components are also considered. The four phases of this program are: (1) Establishment of component specifications and interface requirements for major system components; (2) formulation of alternative sets of conceptual designs for major system components; (3) engineering analysis of various components and systems; and (4) re-examination of basic concept and identification of any desirable follow-up work.
The Langley six degree of freedom visual motion simulator has been used to measure subjective response ratings of the ride quality of eight segments of flight, representative of a wide variation in comfort estimates. The results indicate that the use of simulators for this purpose appears promising. A preliminary approach for the development of criteria for ride quality ratings based on psychophysical precepts is included.
The purpose of this report is to acquaint the Houston community with specific areas of available technology, both public and private, to demonstrate to industry how this technology may be acquired and put to use to provide new and useful services for man. Much of the technology utilized in the development of nuclear-fueled circulatory support systems in our laboratories has evolved from industry, NASA, and AEC; our projects involve radiation biology, thermodynamics, energy transfers, hemodynamics, hematology, pathology, and surgery.
A test program to determine the total discomfort associated with vehicle vibration is described. The program utilizes a three-degree-of-freedom vibration simulator to determine the effects of multifrequency and multiaxis vibration inputs. The approach to multifrequency vibration includes a separate consideration of the discomfort associated with each frequency component or band of the total spectrum and a subsequent empirical weighting of the discomfort components of these frequency bands when in various random combinations. The results are in the form of equal discomfort curves that specify the discomfort associated with discrete frequencies between 1 and 30 Hz and different acceleration levels. These results provide detailed information of the human discomfort response to increases in acceleration level for each frequency investigated. More importantly, the results provide a method for adding the discomfort associated with separate frequencies to give a total typification of the discomfort of a random spectrum of vibration.