The effect of stellar encounters on planetary motions.
Planetary orbit change in major axis, eccentricity and inclination induced by passing star and calculated with central limit theorem
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Planetary orbit change in major axis, eccentricity and inclination induced by passing star and calculated with central limit theorem
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Able-Mars spacecraft bus for Mars entry capsule
Flight test and analysis of structural loads in helicopter hingeless rotor system
Unmanned spacecraft trajectory and guidance considerations for close flyby of planet Mercury
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Study applies the nonequilibrium collision theory of reaction rates to the estimation of rate constants for simple reactions. The complications in the quantum mechanical description of chemical reactions and the care needed in approximating the exact wave function for the collision are shown.
Trajectory optimization for Apollo-type vehicle under entry conditions during lunar return
Quantum mechanical calculations for gas phase bimolecular exchange reactions between hydrogen and bromine
Apollo spacecraft landing simulation to determine impact water pressures, accelerations, and landing dynamics
XB-70 flight tests to determine effect of clear air turbulence
Problems in using probability theory by reliability engineers
Computer program using Monte Carlo methods for simulating solar flares during interplanetary space flight
Experiment payloads for manned space flight missions to Mars and Venus
Rotor-hub bending moment measurements on hingeless rotor helicopter during abrupt maneuvers near ground
Investigation was made of the unstable behavior of a heat-transfer loop operating at a supercritical pressure. Natural convection operation of the loop, with observations on acoustic and slow oscillatory behavior, was emphasized during testing. The basic cause of both types of behavior appeared to originate in the heated boundary layer.
Press kit for Mariner 6 and Mariner 7 Mars flyby missions and TV coverage of surface
Turbine stator blade performance determination from total pressure surveys downstream of blade row, noting problems in pressure measurement