SEARCH · Engineering Papers
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.
Automated drafting system produces schematic and block diagrams from the design engineers freehand sketches. This system codes conventional drafting symbols and their coordinate locations on standard size drawings for entry on tapes that are used to drive a high speed photocomposition machine.
Results from tests of rocket engine for spacecraft reaction control and maneuvering systems
Fast scanning IR microscope for semiconductor evaluation used for engineering design analysis, reliability improvement, failure analysis, etc
Surveyor mission operations, and systems design engineering for Mariner, Voyager, and Surveyor space probes
Engineering design criteria for 30 watts per pound rollup solar array
Orbiting primate spacecraft project planning and documentation on systems design and engineering, experiment design, tests programs, and manufacturing
Specific nuclear light bulb and open-cycle vortex stabilized gaseous nuclear rocket engine designs
Engineering design of transponder system for phase measurement of very low frequency signals
Engineering design data on vehicle-borne subsystems of airborne range and orbit determination system
Engineering design concepts for airborne range and orbit determination transponder station, and test equipment for vehicle and transponder checkout
Integrated supersonic transport engine design for reduced lift connected sonic boom effects
Heterodyne detection in photoconductors, discussing engineering design for high sensitivity in IR
RL-10 and J-2 hydrogen oxygen engine design and development for Saturn Apollo launch vehicles, noting performance parameters from ground and flight tests
Performance and installation data for high bypass ratio turbofan engine designated QE-3
Aerodynamic commercial aircraft engine design for minimum noise level
Design engineering and evaluation of throttlable thrustor system
Aerobell extendible nozzle rocket engine design and performance, cold flow and simulated hot flow test results
Flox/methane pump fed engine, discussing RL-10-1-A engine tests and optimized 5000 lb thrust engine design