Capsule, Gemini #3A, Thermo-Vac Test Article

Thirteen flight-quality Gemini spacecraft were built, but only twelve were launched into space. The thirteenth was spacecraft 3A, which began life as a boilerplate vehicle. Early in 1963 NASA decided it needed a replacement for spacecraft 3, which would be used for the first Gemini manned flight rather than altitude chamber tests. 3A was employed in hatch-opening tests and then was rebuilt as a flight-qualified vehicle, lacking only a heat shield and flight ejection seats. It was subjected to the extreme thermal and vacuum conditions of space in the McDonnell altitude chamber from December 19, 1964, to February 19, 1965, in a test series called Project Orbit. Spacecraft 3A underwent three test runs simulating over 220 orbits, resulting in the modification of the spacecraft coolant system.

The Smithsonian received 3A from McDonnell in 1971 as part of a shipment of surplus Gemini hardware from the military Manned Orbiting Laboratory program.

Transferred from the National Aeronautics and Space Administration

Country of Origin
United States of America

Manufacturer
McDonnell Aircraft Corp.

Date
1964-1965

Type
SPACECRAFT-Manned-Test Vehicles

Materials
Structure: Titanium; cylindrical section: beryllium alloy; conical section: Rene 41 (nickel-steel alloy); heat shield: silicone elastomer
Skin: Beryllium, Nickel Alloy
Dimensions
Overall: 130 in. tall x 89 in. diameter (330.2 x 226.06cm)

Thirteen flight-quality Gemini spacecraft were built, but only twelve were launched into space. The thirteenth was spacecraft 3A, which began life as a boilerplate vehicle. Early in 1963 NASA decided it needed a replacement for spacecraft 3, which would be used for the first Gemini manned flight rather than altitude chamber tests. 3A was employed in hatch-opening tests and then was rebuilt as a flight-qualified vehicle, lacking only a heat shield and flight ejection seats. It was subjected to the extreme thermal and vacuum conditions of space in the McDonnell altitude chamber from December 19, 1964, to February 19, 1965, in a test series called Project Orbit. Spacecraft 3A underwent three test runs simulating over 220 orbits, resulting in the modification of the spacecraft coolant system.

The Smithsonian received 3A from McDonnell in 1971 as part of a shipment of surplus Gemini hardware from the military Manned Orbiting Laboratory program.

Transferred from the National Aeronautics and Space Administration

Country of Origin
United States of America

Manufacturer
McDonnell Aircraft Corp.

Date
1964-1965

Type
SPACECRAFT-Manned-Test Vehicles

Materials
Structure: Titanium; cylindrical section: beryllium alloy; conical section: Rene 41 (nickel-steel alloy); heat shield: silicone elastomer
Skin: Beryllium, Nickel Alloy
Dimensions
Overall: 130 in. tall x 89 in. diameter (330.2 x 226.06cm)

ID: A19711529000