The General Dynamics F-111 Aardvark was a supersonic, medium-range, multi-role aircraft. Developed in the 1960s, it fulfilled a number of roles, including strategic bombing, reconnaissance and electronic warfare. It served with the US Air Force from 1968-96, and saw action during the Vietnam War, as well as other notable military events.
The F-111’s name refers to its look, resembling an aardvark with its long nose. It featured variable geometry wings, an internal weapons bay and a side-by-side cockpit configuration. One particularly unique component was its cockpit, which also served as the aircraft’s crew escape module.
Development of crew escape modules
The F-111 Aardvark’s escape module was a product of the aircraft’s top speed. At Mach 2.2 – or 1,672 MPH – it was believed the component would provide a significant amount of protection for crew members. The self-contained module was itself the cockpit, as well as the upper and forward sections of the spine. It was watertight, which ensured ejections were just as safe at sea as they were over land.
When the module was ejected, following the pulling of the ejection handle, two rocket nozzles separated the part from the rest of the aircraft. Once released, the forward and upper part of the aircraft’s spine acted like a hood, stabilizing the module latterly and longitudinally. A drag chute was then released, slowing the component down, and stabilization and pitch flaps were deployed to help maintain an even descent.
Once the module had decelerated to 300 knots, the recovery chute was released. When deployed, its bridal cables were released, allowing for the module to level out. Impact bags were then deployed at the bottom, ensuring a safe touchdown.