CME-associated Energetic Ions at 0.23 au: Consideration of the Auroral Pressure Cooker Mechanism Operating in the Low Corona as a Possible Energization Process
Explore the source record for details and available documents.
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.
Explore the source record for details and available documents.
Radiometer design and application at 70-gigacycles
Trajectories for return to earth phase of lunar missions
Planetary atmosphere studies i - atomic and molecular processes
Wing and fuselage sheet material for trisonic transports
General instability in shell type structures is a relatively infrequent phenomenon. By general instability is meant that a complete section of a structure becomes elastically unstable, as compared with local crippling or buckling. The first step in design is to rough size the structure and determine its compatibility with air vehicle configuration and system instillations. After this step has been completed, it is possible to survey the layouts to determine whether general instability is likely to occur. The general parameters of length, diameter, frame spacing, element stiffness, etc., are than investigated to determine if a general failing stress exists which is less than any local column, beam column, or panel failing stress. In this way, a well-balanced design is determined and general stability failing modes eliminated.
As the coined name Strato-Lab implies, it is a program which provides a stratospheric laboratory utilizing a plastic balloon platform for manned research investigations. The project was originated in 1954; actual work began early in 1955 and the first manned stratospheric flights were made in 1956. It was conceived and has been continued with the following three objectives: (1) Provide a high-altitude research system, a scientific laboratory, permitting man's active scientific participation (2) Provide an opportunity for studies of man's reactions to an actual environment of physiological and psychological stress (3) Allow an opportunity for man to conduct tests and evaluate specific components and/or techniques in an extremely high altitude environment.
Propellants for lunar landing - high specific and density impulse, ignition, and storage
Fluorescent scattering in planetary atmospheres - ultraviolet spectrum
Lunar surface ballistics, hazards of spacecraft landing or launching, particles - exhaust gases
Methods of improving helicopter efficiency - air- foil characteristics, rotary drive, drag effects
Ground erosion due to vtol downwash
Design and operation of v/stol aircraft with reference to propulsion system noise
Feasible solar probes from present planned vehicle technology - saturn rocket - centaur vehicle
Radiation hazard of heavy galactic cosmic rays - deuteron microbeam study
Space station design - manned space flight
Plasma theory of lewis type bombardment ion engine