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Catalog Data

Manufacturer:
United Aircraft Corporation, Pratt & Whitney Aircraft Division  Search this
Materials:
Pressure Jacket/Support Assembly: Titanium, Stainless Steel, Nickel
Hydrogen Electrode: Nickel
Oxygen Electrode: Nickel and Nickel Oxide
Dimensions:
3-D: 111.8 x 55.9cm, 111.1kg (44 x 22 in., 245lb.)
Type:
SPACECRAFT-Crewed-Electrical Power
Country of Origin:
United States of America
Summary:
The Apollo Command Module primary source of electric power was from a set of three "fuel cells" housed in the Service Module. Each fuel cell combines hydrogen and oxygen to produce electricity and water. The water was used for drinking by the astronaut crew. Each of the fuel cell power plants generates 27 to 31 volts. Normal power output for each power plant is 563 to 1420 watts, with a maximum of 2300 watts.
This particular fuel cell was intended for use in the Apollo Service Module 115/115A, which was schedule for use during the Skylab Program. SM115 was never flown. The unused Fuel Cell was offered to the Smithsonian in 1977 and transferred on April 1978 and immediately loaned to the Oklahoma Center for Science and Arts in Oklahoma City for display.
Credit Line:
Transferred from the National Aeronautics and Space Administration
Inventory Number:
A19780289000
Restrictions & Rights:
Usage conditions apply
See more items in:
National Air and Space Museum Collection
Data Source:
National Air and Space Museum
GUID:
http://n2t.net/ark:/65665/nv908456b8c-2210-4d50-9b45-ed482fc193a0
EDAN-URL:
edanmdm:nasm_A19780289000