Handling Qualities and Trajectory Requirements for Terminal Lunar Landing, as Determined from Analog Simulation
Trajectory requirements for terminal lunar landing from analog simulation of spacecraft
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Trajectory requirements for terminal lunar landing from analog simulation of spacecraft
Description of ground support systems for the surveyor lunar-landing spacecraft
Thermocouples are shipped and stored in hollow plastic hoops. The hoop is an inexpensive but efficient method of protection.
Ported ball valves are sealed under both static and dynamic load conditions by a line-pressure responsive double-acting seal. The top of the seal engages the ported ball at the outer circumferential edge of the seal upper end, and the bottom of the seal seats on a flat circular land with a continuous wall.
Bell X-14A test vehicle used to determine control power and damping requirements for V/STOL AIRCRAFT
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Explore the source record for details and available documents.
Explore the source record for details and available documents.
Procedures for cleaning, decontamination, and encapulation of electronic circuits containing metal-oxide silicon field effect transistors
Flight investigation of control qualities of rudimentary hingeless rotor helicopter
System and equipment descriptions of manned orbital research laboratory, and interplanetary and lunar ferry vehicles
Satellite Telemetry Automatic Reduction System /STARS/ capable of processing data at capacity of 200 million data points per day
ESS telecommunication system concept provides the ability to change according to needs indicated by the data without any change to the lunar experiment equipment. The system will include a magnetic core memory as the data multiplexing control device.
Specially fitted barge is used to load and transport large, heavy objects to a dock side site. There the barge itself can lift, rotate, and position the objects. Typical functions are economically accomplished by water buoyancy.
General purpose digital computer program is applicable for use with analysis programs that require basic data and calculated parameters as input. It is designed to automate input data preparation for flight control computer programs, but it is general enough to permit application in other areas.
Sterilization of spacecraft telecommunications system - pressure transducers, magnetic tape recorders, and magnetic core memories
Computer techniques for data problems encountered by task analysts
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