Publication Date:
2019-06-27
Description:
A feasibility study was conducted on the design and construction of a flight-worthy replaceable battery module consisting of four 100 A.H. nickel-cadmium rechargeable cells for large manned space vehicles. The module is planned to weigh less than 43 pounds and be fully maintainable in a zero-g environment by one man without use of special tools. An active environmental control system was designed for the temperature control of the module.
Keywords:
ENERGY PRODUCTION AND CONVERSION
Type:
NASA-CR-141600
Format:
application/pdf
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