Visibility in space target description subroutine
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Breckenridge, W. T., Jr.↗
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Results for “Description”
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.
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Experimental investigation of the interaction of a plane, oblique, incident-reflecting shock wave with a turbulent boundary layer on a cooled surface. Volume 1 - Test description and data summary
Interaction of plane, oblique, incident reflecting shock wave with turbulent boundary layer on cooled surface - summary
Kilburg, R. F.↗
Analytic description of jet-wake cross sections for a jet normal to a subsonic free stream
Jet-wake cross section analysis for jet exhausting in free stream flow
Margason, R. J.↗
Computer program for crossed-beam studies of clear air turbulence, Program description /MLTCOR/ Final report, 14 May 1968 - 13 Aug. 1969
Computer program for studies of aerodynamic and clear atmospheric turbulence
Phillips, M. R.↗
Description of a General Launch Vehicle Simulation Program and Its Associated Data Program
Equations of motion for load relief analysis and performance evaluation for Saturn 5 class of launch vehicles
Hewitt, G. R.↗
Description of the GDC program for the graphic display of three-dimensional models prepared by the combinatorial geometry technique
Computer programming for graphic display of combinatorial geometry
Guber, W.↗
Description of the VIP program for computing incident and absorbed energy at the surface of an orbiting satellite
VIP program for computing incident and absorbed energy at orbiting satellite surface
Goldstein, R.↗
Description of data plots from the University of Minnesota ion chamber and electron spectrometer on OGO-1 and OGO-3
Samples of electron spectroscopy and ionization chamber data plots from OGO-1 and OGO-3
Kane, S. R.↗
Approximating properties of linear models for input output descriptions
Pade approximations for linear and dynamic programming using Markov processes and new algorithms
Holzmann, E. G.↗
Description and applications of Fluorel L-3203-6
Properties and applications of Fluorel copolymer for nonflammable spacecraft requirements
Supkis, D. E.↗
Description and User's Guide: Gain Initialization Programs GRADGN and LERNGN Final Report, 4 Nov. 1968 - 3 Nov. 1969
Computer programs designed to automatically determine stabilizing feedback for linear time-invariant systems - manual
Mc Brinn, D. E.↗
Introduction - Description of the DSN
Deep Space Network communications, tracking, and ground support facilities and activities
Source record↗
FORMAT 2 - Second version of FORTRAN matrix abstraction technique. Volume 2, supplement 2 - Description of digital computer program system/360 Final report, Jan. - Sep. 1968
FORTRAN matrix conversion for implementing FORMAT 2 on system 360 for airframe structural strain analysis
Hooks, C. G.↗
Study of systems and cost performance methodologies for optimization of vehicle assignment. Volume 1 - Technical description Final report
Cost analysis and computer programs for optimal assignment of expendable and reusable launch vehicles in multi-year, multi-mission space program
Source record↗
A description of the control program for the lunar ranging experiment
Lunar ranging ground station with Varian 620/i control computer
Rayner, J. D.↗
A description of the time interval measurement and laser control circuitry for the lunar ranging experiment
Detector package, laser, and telescopes for lunar ranging experiment
Steggerda, C. A.↗
Theory of collision effects on line shapes using a quantum mechanical description of the atomic center of mass motion - Application to lasers
Quantum mechanical treatment of atomic center of mass motion in theory of collision effects on line shapes
Berman, P. R.↗
Launch Vehicle Description
The Thorad-Agena is a two-stage launch vehicle consisting of a Thorad first-stage and an Agena second-stage, connected by a booster adapter. The composite vehicle, including the shroud and the booster adapter, is about 33 meters (109 ft) long. The total weight at lift-off is approximately 91 625 kilograms (202 000 lbm).
Coffey, E. E.↗