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.