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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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Basic components of system are - occluding cuff with mounted cuff microscope, cuff pump deflator, pressure transducer, preamplifier unit, electrocardiograph machine, an analog to digital convertor unit, and digital display unit. System utilizes indirect auscultatory method, based on Korotkoff sounds, for measurement.
Dual TV monitor and collimated lens system in windscreens of standard aircraft cockpit simulator permits both pilot and copilot to simultaneously view three dimensional presentation. Proper design of complete system permits depth and viewpoint of visual displays to be accurately presented.
Computer programs and predictor displays for solving air traffic control problems
Integrated time shared instrumentation display for aerospace vehicle simulators
Data displays of Radio Astronomy Explorer 1
Reaction times of subjects in tests with display control configurations typical of those used in continuous tracking tasks
VTOL display and control system for deceleration to instrument hover
FORTRAN program for computation of group tables, alphanumeric display
Benefits and problems of using head-up displays in commercial and general aviation aircraft
Cathode ray tube system for displaying ones and zeros in binary wave train
Design and development of flight director systems based on theory of manual control displays
Effect of several variations of two types of TV display visual simulation systems on subjective pilot evaluations and objective measures of performance in landing approach
Plasma-fluidic hybrid display system combining high brightness and memory characteristics
SFOF digital television display subassembly providing continuous television compatible video output
Development and characteristics of display system for space shuttle and cost effectiveness analysis of cathode ray tube system
Design concept for integrated display system suitable for computer management and optimized for pilot acceptability applied to space shuttle
Auxiliary computer routines for generating, checking, and displaying NASTRAN input and output data for analysis of aerospace vehicle structures