TWO APPROACHES TO THE DESIGN OF SPACECRAFT DATA HANDLING SYSTEM
Discussion and comparison of two data handling and control systems for the mariner interplanetary exploration programs
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Discussion and comparison of two data handling and control systems for the mariner interplanetary exploration programs
Microelectronic function blocks and their use in low level amplifiers for space applications
Electronic packaging methods for surveyor spacecraft modules such as the television system, discussing foam sandwich chassis construction and the use of cordwood modules
Design, fabrication and performance of minimum power microelectronic circuits and subsystems
Monostable circuit design satisfies space requirements for minimum power dissipation
Circuits for redundant space-borne systems - detection and location of failure
Radar altimeter for use in Saturn spacecraft
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Analytical design and testing of flip-flop and Nand gate for spacecraft electronic subsystems
Pulsed generator electron tube and semiconductor device minimization and elimination - spacecraft application for all-magnetic logic system
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Magnetic, mechanical, and thermophysical property data on magnetic materials for use in advanced space electric power systems
Low power thin film plated-wire memory unit with nondestructive readout for spacecraft
Data processing of MIT gamma ray telescope aboard OSO-C, particularly packaging having electronic system without single internal cable
Spacecraft RF electronic systems covering voice communications, telemetry, trajectory measurements and digital command system
Cardiovascular and respiratory instrumentation systems for use in physiological measurements on test pilots in high performance aircraft and space flight simulators
NASA space Electronics Research Center noting objectives in guidance, control, communications, instrumentation, data processing and system reliability
Performance characteristics environmentally determined for spacecraft, thin wall wiring