Advanced planetary probe study. Volume 1 - Study approach Final technical report
Study approach to planetary spacecraft designs and missions - spin-stabilized spacecraft design for Jupiter flyby mission in 1972 with 50-lb scientific payload
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Study approach to planetary spacecraft designs and missions - spin-stabilized spacecraft design for Jupiter flyby mission in 1972 with 50-lb scientific payload
Spin-stabilized spacecraft design and functional requirements for Jupiter flyby mission in 1972 with 50-lb scientific payload
Evaluation of 3-axis stabilized, 50-lb science payload spacecraft, Jupiter flyby and orbiter missions, flyby missions to planets beyond Jupiter, capsule entry, and cost effectiveness
Planetary probe conical scanning system, signal processing, S-band power amplifier survey, modulation and bit synchronization, antenna temperature, and trajectory perturbations
Optical technology experiments of Optical Technology Apollo Extension System
Systems integration - Optical Technology Apollo Extension System
Systems integration for Optical Technology Apollo Extension System
Technology development plan, and optical instrument for Apollo project
Hydraulic fluid interaction servovalves - valve design, torque motor specification, environment tests, and vortex valve tests
Diagram method for counting topologies on finite sets
Properties of high field superconductors at high temperatures - magnetization experiments on niobium and niobium compounds
Implementation approaches for conducting Saturn V launch vehicle program without dummy stages
Performance and reliability studies of solar conversion power supply subsystem for Nimbus-B satellite
Statistical evaluation of proton radiation from solar flares
Ganglionic and adrenergic blockade effects on circulatory system studied on young chimpanzee
Threshold studies of phase lock loop systems - effect of phase comparator on overall performance and threshold phenomena
Two-particle spin-orbit nucleon-nucleon interaction of oxygen 16 and nitrogen 16 nuclei
Construction and application of analytical model of wet vapor turbine blad erosion