|A6 3 View|
Credit: Gary Webster. 50,165 bytes. 600 x 442 pixels.
The A6 was designed to further extend the range of the A4b winged rocket through use of a ramjet for cruise propulsion. The A6 was proposed to the German Air Ministry as an invulnerable photo reconnaissance aircraft (anticipating the SR-71 aircraft by twenty years). The rocket engine would accelerate the vehicle to supersonic speed and an apogee of 95 km. After re-entering the atmosphere and beginning the supersonic glide phase, the ramjet would be ignited. Burning synthetic petrol or coal slurry, it provided fifteen to twenty minutes of cruise at 2,900 km/hr. This would have allowed the aircraft to return to base, unlike the A4b. One pilot was provided with a pressurized cockpit. The reusable A6 would be launched vertically but land on a conventional airfield using landing gear and a drag parachute.
|A6 3 view|
Credit: Gary Webster. 57,505 bytes. 300 x 221 pixels.
The A6 designation was also applied to a version of the A5 subscale V-2 using alternate propellants. This had the same dimensions as the A7.
Liftoff Thrust: 12,500 kgf. Core Diameter: 6.3 m. Total Length: 15.8 m.