Lift and cruise engines: complex mechanical construction
The engineers decided against pivoting engines. Instead, they installed wingtip nacelles, each with four Rolls-Royce RB162 turbojets as lift engines—weighing just 127 kilograms a piece but producing two metric tons of thrust. Under each wing, there was a cruise engine equipped with pivoting thrust nozzles, which also aided vertical takeoff. These two engines were Bristol Siddeley (today Rolls-Royce) Pegasus 5-2 turbofans, which were also used in the Hawker Siddeley Harrier—still the most successful V/STOL aircraft ever produced. Not even the most powerful helicopter available at the time had the lift capability of a Do 31 with its maximum takeoff weight of 24.5 metric tons.
On February 10, 1967, the Do 31 took off on its maiden flight from Oberpfaffenhofen near Munich with an initial takeoff weight of 19.3 metric tons. This milestone is made all the more impressive considering that the highly complex challenges concerning the aerodynamics, engine arrangement, flight control and the control-pilot interface were solved using 1960s technology. The control system, which had to manage a precision interaction of lift and cruise engines close to the ground, was a complex mechanical construction. It featured an early version of fly-by-wire, the electronic flight control system, which at the time was being adopted for the Concorde and would later become the backbone of the Airbus cockpit.
Setting still unbroken world records on the way to Paris
The Do 31 came of age in what in any case was a most eventful year in the history of global aerospace. In 1969, both the Concorde and the Boeing 747 had their maiden flights, while the moon landing captivated the world. It seemed anything was possible. Shortly before the moon landing, the Do 31 had set multiple world records for jet-powered vertical takeoff aircraft in its weight class on its ferry flight from Oberpfaffenhofen to the Paris Air Show. One of these was completing the journey in just one hour 19 minutes—a record that has yet to be beaten. Like all vertical takeoff aircraft, however, the Do 31 did have some major drawbacks: it consumed vast amounts of kerosene, which was as objectionable as the noise level both inside and out.
“People in and around Oberpfaffenhofen got scared when the ground shook and they heard the plane’s unbelievable roar, which was nothing like normal aircraft noise,” said German test pilot Dieter Thomas, who died in 2013, in an interview. His colleague Drury Wood, who died in 2019, noted: “This ten-engine aircraft got so incredibly loud that it caused damage.” He was referring to damage to both health and property.
Nevertheless, at the time there were big plans to use vertical takeoff aircraft to transport passengers. Indeed, Dornier had already presented a modified design of the Do 31, dubbed the Do 231. Designed as a shoulder-wing aircraft, the Do 231 was earmarked for Lufthansa as a 100-seater with a maximum speed of 900 km/h and a range of just under 3,000 kilometers. Equipped with a total of 12 lift engines, it could have managed a takeoff weight of 59 metric tons and was set to enter service in 1977/1978.