Control system study Progress report, 8 Sep. - 7 Oct. 1965
Approximate mathematical solutions to space vehicle flight dynamic response control problem
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Approximate mathematical solutions to space vehicle flight dynamic response control problem
Manned orbital research laboratory designed to perform astronomical observations with Cassegrain type telescope
Synchronous orbit study of manned orbital telescope
Vibrophonocardiograph data compared to left ventricular blood pressure, myocardiographic, and electrocardiographic data in dog studies
System for measuring phase stability of very low frequency signal propagated over short distances
Multiple satellite mission analysis, specification requirements and configuration concepts
Standard trajectories and parameters for design of Voyager spacecraft, and performance prediction, interfaces, and reliability of spacecraft subsystems
Two stage bipropellant injection with high thrust per injector
Optimization of VTOL control concepts and comparison on six degree of freedom motion simulator
Engineering design of transponder system for phase measurement of very low frequency signals
Obtaining terrain surface temperatures from radiances measured in orbit
Engineering specifications and prototype model of SS/DSB multiplexer
Design of multispectral scanner for orbital earth resources detection
Design study of digitally programmed supersonic transport flight simulator
Statistical analysis of metric and English unit usage and trends in technical documents generated by NASA Centers
Concepts of control for Outer Planetary Explorer spacecraft
Computer simulation and equations of motion for Apollo 8 crew training for lunar entries
The detail engineering data sheets are presented for all concepts considered in the final phase of the study as well as those only carried through the interim phase due to non-applicability or deleted missions.