WAC Corporal
21. Frank Malina, project leader in the development of the WAC Corporal, stands beside the high-altitude sounding rocket.
The WAC Corporal was the first successful American sounding rocket to reach significant altitude. The first WAC Corporal, launched in 1944 from White Sands Proving Ground in New Mexico, reached a height of 71,600 meters (235,000 feet). The fin-stabilized rocket was powered by a liquid-propellant engine that burned a self-igniting fuel and oxidizer combination. Use of these propellants eliminated the need for an ignition system. By March 1946, these rockets had attained altitudes of over 72.4 kilometers (45 miles) with a booster. The WAC Corporal was later used as a second stage on a German V-2 rocket. This U.S. program, code-named “Bumper,” tested techniques for ignition and separation of stages at high altitudes.
The WAC Corporal was designed in 1944 by the staff of the Jet Propulsion Laboratory, California Institute of Technology.
The rocket on exhibit is from the California Institute of Technology.
| Length | 4.9 m. (16 ft., 2 in.) as exhibited |
| Diameter | 30.5 cm. (12 in.) |
| Fuel | Aniline-furfuryl alcohol |
| Oxidizer | Red-fuming nitric acid |
| Thrust | 680 kg. (1500 lb.) |
| Velocity | 4500 km. (2800 mi.) per hr. at burnout |
| Altitude | 72 km. (45 mi.) with a 11.3-kilogram (25-lb.) payload |