The problem of off duty time in long duration space missions. Volume 1 - Summary and research recommendations
Psychological and social factors in using off-duty time during long-duration space flights
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Psychological and social factors in using off-duty time during long-duration space flights
Simulation objectives and requirements for flight management problems during low visibility approach and landing of supersonic transports
Storability and performance tests on high energy liquid propellants for space missions
Qualitative analysis of spin acceleration effects on solid propellant rocket engine performance
Automatic approach and landing system for V/STOL aircraft
Design and equipment requirements for manned earth orbiting biotechnology laboratory
Storability, thermodynamic properties, and performance of high energy liquid propellants
Basic and applied research in seismology, research and training facilities, users, and funding
Elimination of spurs in Apollo spacecraft telemetry signal transmission
Lunar landmark sighting techniques for Apollo command service module
Lunar orbit insertion abort procedures for hybrid lunar missions
Booklet provides references to 29 publications providing information on hazard control and approved safety practices. Areas include pressurized gas and vacuum systems. Guidelines are presented for safeguarding facilities where machinery, equipment, electrical devices, or hazardous chemicals are used.
Technology and analytical techniques for development of solar power system for space stations
Air pollution monitoring and pollutant source surveillance system, and effective regulations and enforcement means for San Francisco Bay area
Low outgassing polymeric materials for general service and communication satellite structures
Conference report on impact of man on global environment, assessing actions covering climatic and ecological effects, pollution monitoring, etc
An evaluation to determine the compatibility of the Agena with the space transportation system for use as an expendable third stage to the space shuttle was conducted. The Agena was considered for those missions requiring additional propulsion capability beyond that used for low earth orbit. The study defines the interface requirements imposed on both the Agena and the shuttle system and identifies those areas where the Agena must be improved or modified to satisfy mission requirements.
Test requirements and instrumentation are discussed together with a review of general procedures, safety, and maintenance. A term definition listing is included.