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Title
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Propellant-Atmosphere System Study
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Date
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1961
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Index Abstract
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Contrails and DTIC truncated
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Photo Quality
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Not Needed
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Report Number
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WADD TR 60-622
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Corporate Author
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New Devices Laboratories Tapco Group
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Laboratory
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Life Support Systems Laboratory
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Extent
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236
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Identifier
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AD0268768
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AD0268768
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Access Rights
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OTS
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Distribution Classification
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1
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Contract
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AF 33(616)-6514
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DoD Project
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6373
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DoD Task
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63124
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DTIC Record Exists
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No
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Distribution Change Authority Correspondence
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None
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Report Availability
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Full text available
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Full text available
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Date Issued
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1961-03
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Abstract
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Two broad aspects of using chemical energy to provide metabolic oxygen in a manned space capsule were studied: man's ecological requirements and supply of auxiliary power. The studies were restricted to chemicals used in propulsion systems with emphasis on by-products useful to man.
A survey of methods for meeting environmental requirements included (a) evaluation of passive temperature control in terms of capsule size, shape, surface emissivity, orbital altitude, orientation, and internally generated power, and (b) evaluation of weight and energy requirements for supplying oxygen, dehumidifying, and removing CO2 in the cabin.
The best of 40 fuels and 35 oxidizers were screened for other factors: weight of the containers, general methods for converting the energy to electric power, mechanical prime movers (their efficiencies, cycle configurations, weight, specific fuel consumption), thermionic, thermoelectric, and electrochemical conversions. The unique adaptability of the cryogenic hydrogen-oxygen fuel system was demonstrated. This system combined with a hydroxy fuel cell was used in developing a prototype designed to accommodate one man for 3 days and to supply 1 kilowatt of electric power. The prototype included optimization studies of the cryogenic storage system, an air conditioning system, and a fuel cell power system.
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Provenance
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IIT
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Type
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report
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Publisher
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Wright-Patterson Air Force Base, OH : Life Support Systems Laboratory, Aerospace Medical Laboratory, Wright Air Development Division, Air Research and Development Command, United States Air Force
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Subject
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Space Environments
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Space Flight
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Power Supplies
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Spacecraft
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Carbon Dioxide
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Chemical Reactions
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Cryogenics
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Electric Power Production
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Fuel Cells
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Heat Tolerance
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Humidity
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Liquid Rocket Propellants
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Logistics
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Manned
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Mathematical Analysis
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Oxygen
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Physiology
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Rocket Fuels
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Rocket Propellants
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Oxidizers
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Temperature Control
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Format
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1 online resource