Satellite orbital, no. e-7
Tabulated data on SAO mean elements derived from reduced observations
Miller, B.↗
SEARCH · Engineering Papers
Results for “tabulated data”
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
A survey of thermodynamic properties of the compounds of the elements CHNOPS Progress report, 1 Jul. - 31 Dec. 1968
Tabulated data on heats of combustion and heats of formation of organic compounds of biological interest
Armstrong, G. T.↗
Lunar crater counts. III - Post Mare and ''Archimedian'' variations.
Lunar intermare crater density variations data tabulation, presenting quantitative and qualitative estimates
Hartmann, W. K.↗
Venus photographs. I - Photographs of Venus taken with the 82-inch telescope at McDonald Observatory, 1950-56
Venus photographs taken by 82-inch telescope /1950-1956/, tabulating data
Fountain, J. W.↗
Southern Hemisphere meteor rates
Meteor rate data tabulated from controlled parameter radar survey of Southern Hemisphere activity, noting diurnal and annual variations
Ellyett, C. D.↗
Applications Technology Satellites meteorological data catalog, volume 3, 1 February - 31 December 1968
Meteorological data tabulated from Applications Technology Satellites observations including photographs of clouds - Vol. 3
Source record↗
Space Flight Handbooks. Volume 3 - Planetary Flight Handbook. Part 7 - Direct Trajectories to Jupiter, Saturn, Uranus, and Neptune. Supplement A - Tabular Trajectory for Direct Trajectories to Jupiter and Saturn
Direct trajectories to Jupiter and Saturn - data tabulations
Source record↗
Pulsar data tables
Pulsar data tabulation of positions, dispersion measures, and class I pulse periods and widths
Maran, S. P.↗
The brightness of the zodiacal light
Zodiacal light brightness measurement in three mutually perpendicular directions, tabulating data
Roosen, R. G.↗
Space shuttle: Heat transfer rate measurements on Convair booster (B-15B-2) and North American Rockwell orbiter (161B) at nominal Mach number of 8
Plotted and tabulated data from the thin-skin thermocouple phase of an experimental test program are presented. These data are representative of three events of simulated flight and are described as booster-orbiter ascent heating data, booster reentry heating data, and orbiter reentry heating data. The test was conducted in a 50-inch hypersonic tunnel b at a nominal Mach number of 8 and free-stream Reynolds number range of 700,000 to 3,700,000 per foot. The model employed was a 0.009 scale replica of the Convair B-15B-2 booster and North American Rockwell 161B orbiter.
Warmbrod, J. D.↗
Space shuttle: Heat transfer rate measurements on Convair booster (B-15B-2) at nominal Mach number of 8
Plotted and tabulated data on heat transfer from a thin-skin thermocouple are presented. The data is representative of the reentry event of the booster alone configuration. The data were generated during wind tunnel tests of the B-15B-2 delta wing booster at Mach 8. Thermocouple measurements are reduced to heat transfer coefficient ratio and the data are presented as plotted variations versus longitudinal, lateral, and vertical local model positions.
Warmbrod, J. D.↗
Space station program phase B definition: Nuclear reactor-powered space station cost and schedules
Tabulated data are presented on the costs, schedules, and technical characteristics for the space station phases C and D program. The work breakdown structure, schedule data, program ground rules, program costs, cost-estimating rationale, funding schedules, and supporting data are included.
Source record↗
The peculiar star He 2-177 - A slow nova and a possible X-ray source
The remarkable detail resemblence of the spectrum of the peculiar emission-line star He 2-177 to that of the slow nova RR Telescopii is illustrated by tabulated data and discussed. The evolution of the spectrum since 1965 closely resembles the evolution of RR Tel between 1951 and 1954. A newly determined position of X-ray source 2U 1639-62 makes its identification with He 2-177 less probable than before.
Carlson, E. D.↗
Triple balance test of the PRR baseline space shuttle configuration on a .004 scale model of the MCR 0074 orbiter configuration in the MSFC 14 x 14 inch Trisonic Wind Tunnel (TWT 570) IA31F(B), volume 1
A wind tunnel force and moment test of the space shuttle launch vehicle was conducted. The wind tunnel model utilized a triple balance such that component aerodynamics of the orbiter, external tank, and solid rocket booster was obtained. The test was conducted at an angle of attack range from -10 deg to 10 deg, and angle of sideslip range from -10 deg to 10 deg, and a Mach number range from 0.6 to 4.96. Simulation parameters to be used in future launch vehicle wind tunnel tests were investigated. The following were included: (1) effect of orbiter -ET attach hardware; (2) model attachment (spacer) effects; (3) effects of grit on model leading surfaces; and (4) model misalignment effects. The effects of external tank nose shape was studied by investigating five different nose configurations. Plotted and tabulated data is reported.
Ramsey, P. E.↗
Heat transfer tests of a 0.0175-scale space shuttle orbiter model (29-0) to determine the effect of surface temperature on boundary layer transition at Mach 8.0 in the AEDC VKF tunnel B (test OH4A)
Wind tunnel tests were conducted to determine the heat transfer characteristics of a 0.0175-scale model of the space shuttle orbiter and to analyze the effect of wall temperature on the point of boundary layer transition. The tests were conducted at Mach 8.0 over a range of Reynolds numbers from 1.0 to 3.7 million per foot. Two regions of initial model wall temperature were investigated. Eighteen runs were obtained at each region to support the test objectives. Tabulated data are presented along with a description of the test procedure. Preliminary data indicated that the initial model wall temperature did not obviously affect the point of boundary layer transition.
Foust, J. W.↗
Heat transfer phase change paint tests of 0.0175-scale models (nos. 21-0 and 46-0) of the Rockwell International space shuttle orbiter in the AEDC tunnel B hypersonic wind tunnel (test OH25A)
Tests were conducted in a hypersonic wind tunnel using various truncated space shuttle orbiter configurations in an attempt to establish the optimum model size for other tests examining body shock-wing leading edge interference effects. The tests were conducted at Mach number 8 using the phase change paint technique. A test description, tabulated data, and tracings of isotherms made from photographs taken during the test are presented.
Dye, W. H.↗
An analytic method to account for drag in the Vinti satellite theory
A quadrature algorithm is presented which employs analytical expressions for the variations of satellite orbital elements caused by air drag. The Hamiltonian is formally preserved and the Jacobi constants of the motion are advanced with time through the variational equations. The atmospheric density profile is written as a fitted exponential function of the eccentric anomaly, which adheres to tabulated data at all altitudes and simultaneously reduces the variational equations to definite integrals with closed form evaluations, whose limits are in terms of the eccentric anomaly. Results are given for two intense air drag satellites and indicate that the satellite ephemerides produced by this method in conjunction with the Vinti program are of very high accuracy.
Watson, J. S.↗
Minor planets and comets in libration about the 2:1 resonance with Jupiter
We examine the orbits of minor planets in a search for objects librating about the 2:1 mean-motion resonance with Jupiter. Some 30 candidates are found among the Palomar-Leiden Survey and other unnumbered minor planets. Although almost all the orbits are very uncertain, there does seem to be an indication that librators of low orbital eccentricity do exist, contrary to the hypothesis by Giffen. We also tabulate data describing 12 comets that are temporarily librating about the 2:1 resonance. Finally, we present a discussion of what are apparently 'apocentric' librations. This type of libration, of which we find seven representatives among the numbered minor planets, can occur only for sufficiently small eccentricity. For such bodies, the role of Jupiter's eccentricity is vital; it is associated with a continuing alternation between apocentric libration and an oscillation of the line of apsides.
Franklin, F. A.↗