Accuracy of modal stress calculations by the finite element method
Geometrically exact finite element for thin shells of revolution, using approximation to predict boundary layer stress distribution during vibration
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Geometrically exact finite element for thin shells of revolution, using approximation to predict boundary layer stress distribution during vibration
Film reduction and time keeping used at Smithsonian Astrophysical Observatory for Baker-Nunn films
Bits quantity required to represent coefficient within digital controller with high sampling rate
Low altitude atmospheric effects on IR beam horizon sensors in carbon dioxide band, noting corrections for spacecraft attitude measurement
Preflight error statistics of earth based Doppler tracking for Mariner navigation concerning Mars 1971 and Venus-Mercury 1973 missions
Limit analysis for ionization potential reduction effect on ionized gas atomic composition, considering temperature and electron density
Test program to verify theory used in calculating axial thrust uses turbopump instrumented with /a/ proximity transducers for measuring shaft position, /b/ a strain gage thrust bearing carrier to measure axial thrust, and /c/ internal pressure taps to define component pressure gradients used in thrust calculations.
Computer program for predicting structural bending vibrational data
Sequential estimation with process noise for processing DSN tracking data during planetary orbiter missions and Doppler determinations of polar motion using satellites
Shuttlecraft landing and navigational aid capabilities
Data processing methods for improving FPS-16 radar/Jimsphere system measurements of atmospheric motion
Procedures for accurate condensing of eigenvalue solutions in structural analysis using Guyan reduction solutions
Satellite skin potential and errors in electron density and temperature determinations by Langmuir probe measurements, using model ionosphere
Spectral scanning method for determining temperature profile of jet- or rocket-engine exhaust stream by gas radiation and transmittance measurements, discussing radiometric errors effects
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A brief discussion of the actual laser tracking performance of geodetic satellites is followed by a discussion of the errors inherent in the laser system. An estimate is made of the capability expected within the next few years for the tracking of a heliocentric probe. The GEOS 1, GRARR, and GEOS 2 systems are considered. Errors in the tracking of a heliocentric probe are noted. These include errors due to the earth's atmosphere, (beam bending, atmospheric absorption, atmospheric turbulence, and atmospheric distortion of short laser pulses), and errors due to coronal effects.
Motion in the general gravity field is described mathematically. A covariance analysis, based on two simple models, is presented. Two drag-free space probes were considered, for which the orbital elements are given.
The spectral-scanning method may be used to determine the temperature profile of a jet- or rocket-engine exhaust stream by measurements of gas radiation and transmittance, at two or more wavelengths. A single, fixed line of sight is used, using immobile radiators outside of the gas stream, and there is no interference with the flow. At least two sets of measurements are made, each set consisting of the conventional three radiometric measurements of absorption-emission pyrometry, but each set is taken over a different spectral interval that gives different weight to the radiation from a different portion of the optical path. Thereby, discrimination is obtained with respect to location along the path. A given radiometric error causes an error in computed temperatures. The ratio between temperature error and radiometric error depends on profile shape, path length, temperature level, and strength of line absorption, and the absorption coefficient and its temperature dependency. These influence the choice of wavelengths, for any given gas. Conditions for minimum temperature error are derived. Numerical results are presented for a two-wavelength measurement on a family of profiles that may be expected in a practical case of hydrogen-oxygen combustion. Under favorable conditions, the fractional error in temperature approximates the fractional error in radiant-flux measurement.