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This is a Suit and Cabin Temperature Control Valve used in the Gemini program. Mounted between the two ejection seats, the dual concentric knobs turned by the astronauts controlled the operation of valves regulating the flow rate of primary and secondary coolant through the suit and cabin heat exchangers. Clockwise rotation resulted in increased temperatures. There is no indication that this valve was ever flown in space and it was probably used for testing. Airesearch Mfg. Co. made the valve and NASA transferred it to NASM in 1969.
Display Status
This object is not on display at the National Air and Space Museum. It is either on loan or in storage.
Object Details
Country of Origin
United States of America
Type
EQUIPMENT-Miscellaneous
Manufacturer
Airesearch Dimensions
3-D: 15.9 x 18.4 x 11.4cm (6 1/4 x 7 1/4 x 4 1/2 in.) Materials
Anodized Aluminum
Steel
Cadmium Coating
Chrome Plating
Paper
Ink Inventory Number
A19700354000
Credit Line
Transferred from the National Aeronautics and Space Administration
Data Source
National Air and Space Museum
Restrictions & Rights
Usage conditions apply
For more information, visit the Smithsonians Terms of Use.