Voyager spacecraft system. Management philosophy and program highlights Final technical report
Design concepts, management philosophy and program highlights of research toward Voyager spacecraft development
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Design concepts, management philosophy and program highlights of research toward Voyager spacecraft development
Design and performance characteristics of rocketborne instrumentation system to measure radio frequency noise energy
Optical communication equipment design and integration - propulsion subsystem - guidance, navigation, and environmental control
Design calculations and materials test data for planetary entry ringsail parachute
Design and operational performance of solid state ultrahigh frequency prototype telemetry transmitter
Design parameters for developing phased array acquisition and tracking radar for onboard experiment in Apollo spacecraft
Design and fabrication of electronic pressure switches
Design and tests of MHD induction generator operating on liquid flow
Design characteristics of universal position switches for Launch Complex 39 service arm
Design and development of electrical system and power conditioning equipment for thermoelectric outer planet spacecraft program
Design and construction of system for measuring frequency of S band, FM TV transmitter
Various studies and analyses that were performed in support of the V/STOL research transport design effort are discussed. The propulsion system specified for these studies was the LF460/YJ97-GE-100 turbotip lift fan. Strong emphasis was placed on achieving low fan noise while maintaining the high thrust/weight capability of the high pressure ratio lift fan system. The work was divided into cycle analysis and performance studies, installation and systems support, acoustic analysis and preliminary or conceptual design studies.
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Triadic digit reader and printer for automatic data processing system
Performance prediction and design analysis of constricted coaxial-flow arc air heaters for materials testing and atmospheric entry simulation
Performance evaluation of plutonia fueled multicell thermionic converter
Capacity of holographic memory system with laser system, acousto-optic beam deflector, block data composer and synchronizer
Design and fabrication of conical wheels for lunar surface vehicle