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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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Intermediate thrust sub-arcs analyzed by method of characteristic constants for optimum retrothrust program in inverse-square-law force field
Magnetic annular arc thrust and current-voltage characteristics, using various working fluids
Numerical method to obtain pressure distribution on arbitrary wing planform of various surface shapes with attention to aerodynamic characteristics
Aerodynamic characteristics of spherically blunted cones at Mach numbers from 0.5 to 5.0
Static and propulsive performance characteristics of ducted fan at zero angle of attack for several fan blade angles
Effects of wing planform on aerodynamic characteristics in pitch and sideslip of wing-body-tail model at supersonic wind tunnel speeds
Surveyor Lunar Roving Vehicle /SLRV/ system description and performance characteristics
Static aerodynamic characteristics of rocket model vehicles with thick wedge fins with sweptback leading and trailing edges - supersonic wind tunnel testing of vehicle longitudinal stability
Critical flow characteristics and pressure ratios of sodium vapor flowing through axisymmetrical convergent-divergent nozzle
Nozzle expansion and flow characteristics of potassium vapor
Aerodynamic characteristics of reentry body - pressure distribution at angles of attack and trajectory analysis
Static longitudinal aerodynamic characteristics of sharp right circular cone at Mach 20.3 and angles of attack to 110 deg in helium
Engine nacelle orientation effect on aerodynamic characteristics of arrow wing body configuration
Wing-slope positive ion temperature measurement technique for Langmuir probe volt-ampere characteristic analysis
Aerodynamic characteristics determined for vertical and/or short takeoff and landing /V/STOL/ tilt-wing, multiengine aircraft
Aerodynamic characteristics of scale model of X-15 research aircraft determined in transonic pressure tunnel
Solar simulator performance characteristics effects on spacecraft heat test
Full-scale power-off flight lift and drag characteristics of X-15 aircraft
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