The effects of coriolis acceleration during zero-gravity parabolic flight.
Hematology and biochemical stress effects of coriolis acceleration during zero-gravity parabolic flight
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.
Hematology and biochemical stress effects of coriolis acceleration during zero-gravity parabolic flight
Satellite tracking system accuracy analysis for parabolic antenna - satellite motion, wind, and noise - spectrum effects
Numerical calculation of Weber parabolic cylinder functions - Lie series formalism
Wave propagation in random plasma medium with inhomogeneous parabolic electron density profile background for ionospheric propagation applications
Large space parabolic expandable truss antenna experiment
Parabolic expandable truss antenna experiment design for Apollo applications program
Apollo Applications Program parabolic antenna experiment to evaluate large space structures and extravehicular activities
Cosmonauts inversion illusion in parabolic flight studied with normal and deaf subjects, noting probable dependence on otolith function
Volterra and partial differential equations solution asymptotic behavior treated, indicating connection to boundary problems in parabolic equations and optimal control
Behavioral reactions of unrestrained normal and labyrinthectomized squirrel monkeys to repeated zero gravity parabolic flight simulation, noting initial disorientation and acclimatization
This report covers a comprehensive research study of Androforming, explosive forming, and stretch forming as applied to shaping a parabolic reflector segment for use in a solar furnace. Development efforts were directed toward attaining accurate part contour, and assurance of process reproducibility. The three forming processes mentioned above were investigated by qualified contractors. Three test segments formed by each method along with a detailed analysis were submitted to MSFC. It was concluded that optimum results could be obtained with the stretch forming process. The three test segments of the solar concentrator tha.t were produced by this method, and evaluated optically, revealed a maximum contour deviation of O. 76 degrees.
Solution of first boundary value problem for parabolic equation using power series method
Motion sickness susceptibility under weightless and hypergravity conditions generated by parabolic flight
Human motion sickness susceptibility when exposed to Coriolis accelerations during parabolic flight weightlessness
Radiation patterns for thermally distorted, 30 ft Applications Technology Satellite parabolic antenna computed using digital techniques
Optimal control of system governed by linear parabolic equation with white noise inputs, using mathematical model to generate distributed system analog
Boundary value problem for elliptic-parabolic partial differential equations in theory of random processes, obtaining analytical solution in terms of hypergeometric functions