Skip to main content Smithsonian Institution

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's 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 contain 31 separate cells connected in series. Each cell has hydrogen and an oxygen compartments and electrodes, which in combination produce 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 installed in Service Module (SM) 102 during ground testing and operations conducted at the module's North American Aviation manufacturing site in California. It was transferred to the Smithsonian in September 1972. SM-102 was not flown.
Credit Line:
Transferred from NASA, Johnson Space Center.
Inventory Number:
A19730934001
Restrictions & Rights:
CC0
See more items in:
National Air and Space Museum Collection
Data Source:
National Air and Space Museum
GUID:
http://n2t.net/ark:/65665/nv9e4cc07a9-4f73-4e67-8af9-d3cf2706a6e7
EDAN-URL:
edanmdm:nasm_A19730934001