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Results for “Representatives” 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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At least 523 records · Page 29NASA NTRS 1962
Statement of nasa administrator before house committee on science & astronautics - nasa programs, space science, astronautics
NASA NTRS 1962
Nasa aeronautical research program - helicopters, supersonic transport, stol vehicles, multimission aircraft & x-15 - congressional hearings
NASA NTRS 1963
Periodic solution of restricted three body problem as analytic continuation of keplerian elliptical motions
NASA NTRS 1963
Chronology of astronautical and aeronautical events of 1962
NASA NTRS 1963
Nasa appropriations hearing before committee on science and astronautics
NASA NTRS 1963
Restricted three-body problem is solved using solutions of eulers problem of two fixed centers
NASA NTRS 1964
Takeoff performance of supersonic transport configurations
NASA NTRS 1966
Regression curves computed from urinary calcium excretion and bone mass data obtained from men in bed rest and ambulatory studies
NASA NTRS 1959
Transonic wind tunnel study of static longitudinal and lateral stability and control characteristics and drag rise of fighter aircraft
STATIC STABILITY AND CONTROL ↗ NASA NTRS 1966
Effects of multimode and damping on random fatigue of cantilever beams and brackets
NASA NTRS 1967
Computer production runs of low energy intranuclear cascade calculation in graphical form
NASA NTRS 1966
Aerodynamic characteristics of parachute fabrics at simulated high altitudes
NASA NTRS 1968
Boiler design for potassium and cesium Rankine cycle space power plants
NASA NTRS 1969
Load and temperature effects on fatigue strength of notched titanium alloy sheet for supersonic transport operation
NASA NTRS 1969
Shock and vibration characteristics of panel van with spring suspension system
NASA NTRS 1970
Launch windows for Mars departures from elliptical orbits and associated propulsive velocity requirements
NASA NTRS 1970
Longitudinal aerodynamic stability of three hypersonic aircraft at Mach numbers from 0.065 to 10.70
NASA NTRS 1970
Plane wave reflection decay rate representation by slowness diagrams