Description of vehicle system and flight tests of nine trailblazer i reentry physics research vehicles
Flight tests of trailblazer i reentry vehicles
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Flight tests of trailblazer i reentry vehicles
Capability of lateral control system to provide aerodynamic heading-angle control of vehicle having maximum lift-drag ratio during reentry
Spectrogram of visible radiation emitted from trailblazer ii reentry vehicle
Approximate solutions for flight path angle of reentry vehicle in upper atmosphere
Earth reentry vehicle for use in manned mars mission
Rocketborne spectroradiometer measurement of spectral radiation intensity of luminescent air in shock induced flow field produced by reentry vehicle
Trailblazer II reentry physics research vehicle
Effect of aerodynamic characteristics of nose bluntness on electromagnetic and luminous efficiency by comparing radar and optical data of two reentry bodies at escape velocities
Thermal sensors for measuring surface temperature and heat flux on glide reentry vehicles
Convective and equilibrium radiation heat transfer prediction for Project Fire reentry vehicle
Miniature data storage system for missile reentry heat data
Reduction of free electron concentration in reentry plasma by liquid injection
Analog simulation of piloted Earth reentry at parabolic velocity to determine pilot ability to control spacecraft and perform long and short range navigation tests
Data reduction approximation of reentry angles of attack from rate-gyro and accelerometer data
Review of piloted atmospheric reentry simulation studies in general research and in support of X-15 and Mercury projects - fixed cockpit simulators
Observation of GT-5 rocket body reentry - preliminary analysis of second stage of Titan launch vehicle
Aerodynamic characteristics of reentry body - pressure distribution at angles of attack and trajectory analysis