Description and applications of Fluorel L-3203-6
Properties and applications of Fluorel copolymer for nonflammable spacecraft requirements
Supkis, D. E.↗
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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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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.↗
Description and performance of the Saturn launch vehicle's navigation, guidance, and control system
Analysis of Saturn launch vehicle navigation, guidance, and control system
Haeussermann, W.↗
MCC/GSFC/RS General Description
Apollo real time computer complex, remote site equipment, and communications, command, and telemetry system
Source record↗
Description of the SERT 2 spacecraft and mission
Performance and orbital flight plan of SERT 2 ion thruster spacecraft
Goldman, R. G.↗
Description and general operating guideline for KSC lightning warning system
Lightning warning system of Kennedy Space Center
Source record↗
Analyses for the description of rocket and airbreathing propulsion system combustion chamber and nozzle flows Annual report
Calculations of rocket and air breathing propulsion system combustion chamber and nozzle flow performance
Edelman, R. B.↗
Description of a digital computer program for airplane configuration plots
Digital computer program for aircraft configuration plotting
Craidon, C. B.↗
AMTRAN system design and software description
Automatic Mathematical Translation language software for IBM 1130
Dyer, M. E.↗
Localized orbital description of the C-O bond in ketene
Bonding scheme of C-O in ketene described by localized orbital technique
Del Bene, J.↗
A small animal acto-ballistocardiograph - Description and illustrations of its use
Actoballistocardiography based on piezoelectricity for biorythmic activity, respiratory movements and heart rate of small animals
Rogallo, V. L.↗