Ranger tv subsystem /block iii/. volume 4b- appendices
Component reliability and failure analysis of Ranger television subsystem
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Component reliability and failure analysis of Ranger television subsystem
Evaluation of Ranger television subsystem - flight model performance
Ranger VII flight summary and discussion of lunar surface photographs
Earth based radio tracking and orbit determination accuracies for Ranger and Mariner missions
Six-camera two channel television subsystem designed for use in Ranger VI through IX SPACECRAFT
Mariner Venus and Ranger tracking, examining quantization and transmitter stability as dominant effects in HF noise component of Deep Space Instrumentation Facility /DSIF/ L-band Doppler
Ranger lunar probe photograph analysis, crater size and shape measurements and dominant topographic features including camera and command systems
Ranger VII satellite instrumentation system with details on design, performance, flight and results
Rangers VI through IX TV subsystem testing under simulation of Atlas and Agena launch characteristics, midcourse motor action and deep space environment
Earth based radio tracking and orbit determination accuracies for Ranger and Mariner missions
Ranger lunar observation program objectives and accomplishments
Ranger III flight path and its determination from tracking data
Extensive vibration measurements from ground test acoustic simulations of Ranger spacecraft launch, and transonic vibration excitation modes
Vibration tests on Ranger spacecraft with single point control of input vibratory accelerations
Design, development, and flight operation of midcourse propulsion system used on Ranger Block III spacecraft
Selenographic and geologic interpretations of lunar photographs from Ranger Block III