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.
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Capability of lateral control system to provide aerodynamic heading-angle control of vehicle having maximum lift-drag ratio during reentry
Age forming aluminum for center piece head of Saturn S- IC stage
Apparatus for measuring static friction between magnetic tape and heads of tape recorders
Head-end steering for simplified manned launch vehicle
System optimization of head-end steering for manned space vehicle
Limits of head wave amplitudes for short spreads from charges, blasting caps, and 45-kilogram weight drops
Sound pressure in external auditory meatus and near center of cat head in absence of animal as function of frequency
Manipulator operator uses an improved resolution tv camera/monitor positioning system to view the remote handling and processing of reactive, flammable, explosive, or contaminated materials. The pan and tilt motions of the camera and monitor are slaved to follow the corresponding motions of the operators head.
Nonnewtonian mathematical model and plotting method for analyzing variable head viscometer data obtained on pseudo-plastic polymer solutions - Rheology
Egocentric localization of visual horizontal in normal and labyrinthine-defective observers as function of head and body tilt
Head mounted electron guidance platform construction and error analysis, noting stereotactic accuracy
Egocentric localization of visual horizontal in normal and labyrinthine defective observers for various head and body tilts
Time response correlation of vestibular adaptation in slow rotating environment with directed head movements
Excitation and detection circuitry for flux responsive magnetic head
Head movements controlled for rapid vestibular adaptation in slow rotation room /SRR/, preventing motion sickness
Streamline calculations for tandem row high head pump inducers
Head to base transfer function characteristics of partially filled cylindrical propellant tank