Drawn up as a possible all-weather and night-fighter, the P.1079B was the natural progression of a line of design studies undertaken by Heinkel engineers during the latter World War 2 (1939-1945) period that began with the P.1079A (detailed elsewhere on this site) of early-1945. In its original form, the aircraft carried a two-person crew (seated in tandem, back-to-back) and the aircraft sported large, swept-back wing mainplanes along with a "V-tail" plane arrangement. A side-by-side twin engine configuration would power the machine.
In the "P.1079B" revision, the aircraft was modified extensively by becoming a near-flying-wing design. The larger surface area of the delta-wing arrangement meant that no horizontal tailplanes were needed. The V-tail was given up in favor of a more traditional single fin. Furthermore, the wing mainplanes, sweptback at 45-degree angles, were now cranked to become "gull-wing" in form, giving the possible fighter a futuristic appearance. Again a twin turbojet engine configuration would be used for propulsion and a tricycle undercarriage for ground-running. The crew was reduced to a single person in this new design approach and his position was set under a lightly-framed cockpit near the nose of the aircraft. Each engine was aspirated through a circular intake located at each wing root and would be exhausted near the wing trailing edges, ahead of the tail unit. Structural measurements included a running length of 29.6 feet and a wingspan of 42.8 feet.
Power would come from 2 x Heinkel Hirth HeS 011 turbojet engines providing for an estimated maximum speed of 630 miles-per-hour.
In any event, the P.1079B was not progressed any further than paper drawings and may have been a product of the early post-war period following the capitulation of Germany in May 1945.
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AIR-TO-AIR COMBAT
General ability to actively engage other aircraft of similar form and function, typically through guns, missiles, and/or aerial rockets.
INTERCEPTION
Ability to intercept inbound aerial threats by way of high-performance, typically speed and rate-of-climb.
X-PLANE
Aircraft developed for the role of prototyping, technology demonstration, or research / data collection.
29.5 ft (9.00 meters) Length
42.7 ft (13.00 meters) Width/Span
13.1 ft (4.00 meters) Height
11,023 lb (5,000 kilograms) Empty Weight
22,046 lb (10,000 kilograms) Maximum Take-Off Weight
+11,023 lb (+5,000 kg) Weight Difference
2 x Heinkel HeS 011 turbojet engines developing 2,866lb of thrust each. Propulsion
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