A counterbalance system for dynamic testing of equipment designed to operate in a zero-g field.
Counterbalance system using a servomechanism, for dynamic testing of equipment operating in a zero-g field
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Counterbalance system using a servomechanism, for dynamic testing of equipment operating in a zero-g field
Test to determine minimum temperature difference between heated wall and liquid hydrogen at boiling point required to initiate nucleate boiling under steady state conditions and zero-g.
Zero-g docking simulators for testing support mechanisms
Basic physical/biological phenomena studied under zero-g conditions in Earth orbital spacecraft
Drop and aircraft tests to study film boiling of liquid hydrogen at zero gravity
Zero gravity satellite concept feasibility and control system design evaluation using air cushion vehicle
Feasibility of stability and gravity experiments for manned orbiting missions
Bubble accumulation in simulated boiling at zero gravity using Centaur tank model
Sloshing effects of liquid-hydrogen fuel on tank outflow during Centaur engine chill down
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Synergistic effect of weightlessness and radiation on white blood cells during Gemini 3 mission
Communication system for connecting nine personnel stations and public address system for underwater operations - zero G simulation
Food packaging and handling under zero-g conditions of space
Zero-g simulation by parabolic aircraft flight for astronaut training
Development status of regenerable life support system compatible with zero-g, employing physical chemical processes for sustaining crew during space flight simulation
One of the most important and probably the most interesting phase of a manned lunar mission will be the time the astronauts spend outside their vehicle on the moon's surface taking scientific measurements, exploring the surface features, surveying possible sites for a lunar base, inspecting their vehicle and preparing it for their return trip. Because the lunar gravity is only one-sixth that of the earth gravity, the explorers undoubtedly will have to adjust their accustomed methods of walking, climbing, jumping and performing other self-locomotive activities in order to carry out these various tasks. In as much as the over-all success of the lunar mission will depend to a large extent upon the self-reliance of the explorers, it will be necessary to have extensive knowledge of the effects of the moon's reduced gravity on the physical capabilities of man and of man's ability to adopt to the new environment prior to the planning and execution of the mission. At the present time there is a dearth of information on this subject due primarily to the lack of a practical technique for simulating the reduced gravity. Several techniques such as immersion in water and riding in an airplane flying a Keplerian trajectory have been used for zero-g or weightlessness studies to determine the physical capabilities of man but these techniques are limited in their usefulness either by restrictions imposed by the viscous effect of the water or by the short duration and small test area available in an airplane. Consequently, an effort was made at the NASA Langley Research Center to devise a new technique that would provide a realistic simlation of a reduced gravity for unlimited periods of time and allow freedom of movement over considerable distances. This paper concerns itself with a discussion of the newly developed simulation technique and a presentation of some preliminary results which were obtained utilizing a working model based on this scheme.
Zero-g vapor feed system with no moving parts, noting ion engine testing, propellant use efficiency and surface tension storage
Surface tension propellant storage and feed systems for zero-g ion engines