The lunar orbiter telecommunications system.
Spacecraft and ground equipment design of lunar orbiter telecommunications system
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Spacecraft and ground equipment design of lunar orbiter telecommunications system
Zero-gravity mercury feed system for mercury- electron bombardment spacecraft engines
Continuous loop magnetic tape recorders used in Vanguard, Tiros and Nimbus satellites
Centralized Flexible Automatic Computer Telemetry System /FACTS/ for spacecraft, providing capability of revising sampling structure
Small scientific satellite PFM telementry encoding system evolution
Sterilization of spacecraft telecommunications system - pressure transducers, magnetic tape recorders, and magnetic core memories
Bibliography and new techniques for use of error correction and redundancy to improve reliability of spaceborne computers
Hybrid tunnel-diode/transistor integrated circuit squaring counter system for spacecraft
Onboard computers for pre-transmission data processing, automation of data acquisition centers, and real time data relay to control centers for advanced space information systems
Spacecraft data system with stored program computer
Component reliability and machine language features of onboard spacecraft digital computer
Metallurgical methods for detection and analysis of failure mechanisms in microelectronic devices
Electrostatically focused klystron development for use in interplanetary spaceborne communication systems
Fabrication and testing of high-efficiency 100 W S-band traveling wave tube for spacecraft application
Vibrating-piston electrostatic field sensor for Gemini program, examining design improvements including unity-feedback preamplifier, noise reduction devices, etc
Onboard checkout equipment design requirements, considering hardware and software for manned spacecraft flight
TV camera to be used by Apollo astronauts noting integrated circuits, optical system, light intensifier, etc
Relay failure in spacecraft subsystem analyzed via vibration testing