Summary of VGH data collected on one type of twin-engine jet airplane during airline operations
Summary of vertical gusts acceleration data collected for one type twin engine jet airplane during airline operations
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Summary of vertical gusts acceleration data collected for one type twin engine jet airplane during airline operations
Test program summary for Apollo Applications Program combined mission payload integration
Summary information on technical activities of deep space network, space flight projects, communication systems, and deep space instrumentation facilities
Photographic summary report of Lunar Orbiter 4 mission. The fourth of five Lunar Orbiter spacecraft was successfully launched from Launch Complex 13 at the Air Force Eastern Test Range by an Atlas-Agena launch vehicle at 22:25 GMT on May 4, 1967. Tracking data from the Cape Kennedy and Grand Bahama tracking stations were used to control and guide the launch vehicle during Atlas powered flight. The Agena-spacecraft combination was boosted to the proper coast ellipse by the Atlas booster prior to separation. Final maneuvering and acceleration to the velocity required to maintain the 100-nauticalmile- altitude Earth orbit was controlled by the preset on-board Agena computer. In addition, the Agena computer determined the maneuver and engine-burn period required to inject the spacecraft on the cislunar trajectory 20 minutes after launch. Tracking data from the downrange stations and the Johannesburg, South Africa station were used to monitor the boost trajectory.
Summary of government research projects on sonic boom generation, propagation and minimization
Selected photographs and mission summary of Lunar Orbiter 5. The last of five Lunar Orbiter spacecraft was successfully launched from Launch Complex 13 at the Air Force Eastern Test Range by an Atlas-Agena launch vehicle at 22:33 GMT on August 1, 1967. Tracking data from the Cape Kennedy and Grand Bahama tracking stations were used to control and guide the launch vehicle during Atlas powered flight. The Agena-spacecraft combination was boosted to the proper coast ellipse by the Atlas booster prior to separation. Final maneuvering and acceleration to the velocity required to maintain the 100-nautical-mile-altitude Earth orbit were controlled by the preset on-board Agena computer. In addition, the Agena computer determined the maneuver and engine-bum period required to inject the spacecraft on the cislunar trajectory about 33 minutes after launch. Tracking data from the downrange stations and the Johannesburg, South Africa station were used to monitor the boost trajectory.
Summary data on development, fabrication, and testing of exploding bridgewire pressure cartridge
Summary of designs, requirements, constraints, and references for Mars hard lander study system
Space Programs Summary - supporting research and advanced development
Design, fabrication, and testing of 12-kilowatt inductor alternator, voltage regulator-exciter, and parasitic loading speed controller - summary
Final technical summary report on fabrication, delivery, and installation of Saturn S-5 ground computer system
Conference summary - selected NASA technology in electric power industry utilization
Summary of methodology and results of study of space power systems
Voice broadgast mission study - summary
Mars spinning support module mission study, summary data
Summary of random vibration prediction procedures for aerospace vehicles, with bibliography
Summary data on methodology, mission and vehicle criteria for parametric study of manned life support systems
Parametric analysis of microwave and laser systems for communication and tracking - summary