Initial results of studies of handling qualities of a simulated lunar landing vehicle
Initial flight results and description of facility for simulating lunar landing vehicle control
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Initial flight results and description of facility for simulating lunar landing vehicle control
Optimum values of pitch rate damping, longitudinal control and speed stability for vertical takeoff aircraft /helicopters/ using pilot ratings
Rocket-borne spectrometer for solar X ray detection and analysis
Satellite digital video data analyzed by two dimensional filter computer technique, discussing biomedical applications
Approach and landing performance of XB-70 aircraft
Dynamic characteristics of aircraft with wings free to pivot spanwise axis
Real-time ground processing of space mission telemetry data from orbiting telescopes
Linear multivariable feedback control systems design method based on transfer matrix, testing decoupling desirability
Fixture holds flat conductor cable and wires in position until after soldering of contacting conductor ends and potting of junctions. Device provides for proper spacing of wires and adequate access for soldered joints during fabrication, and positions mold halves during potting operation.
Computer programming requirements in support of solar astronomy experiment on manned space station
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AUPLOT 2, set of callable subroutines for computer graphics
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Aerodynamic stability control for reentry trajectory of space shuttle orbiter at transition maneuver
Device which separates and screens particles of soil samples for vidicon viewing in vacuum and reduced gravity environments
Pre-processor, post-processor, and multiple level substructuring routines for data management in support of NASTRAN finite element structural analysis of spacecraft