Propellant-Atmosphere System Study

Item

Title
Propellant-Atmosphere System Study
Date
1961
Index Abstract
Contrails and DTIC truncated
Photo Quality
Not Needed
Report Number
WADD TR 60-622
Corporate Author
New Devices Laboratories Tapco Group
Laboratory
Life Support Systems Laboratory
Extent
236
Identifier
AD0268768
AD0268768
Access Rights
OTS
Distribution Classification
1
Contract
AF 33(616)-6514
DoD Project
6373
DoD Task
63124
DTIC Record Exists
No
Distribution Change Authority Correspondence
None
Report Availability
Full text available
Full text available
Date Issued
1961-03
Abstract
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.
Provenance
IIT
Type
report
Publisher
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
Subject
Space Environments
Space Flight
Power Supplies
Spacecraft
Carbon Dioxide
Chemical Reactions
Cryogenics
Electric Power Production
Fuel Cells
Heat Tolerance
Humidity
Liquid Rocket Propellants
Logistics
Manned
Mathematical Analysis
Oxygen
Physiology
Rocket Fuels
Rocket Propellants
Oxidizers
Temperature Control
Format
1 online resource