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Aviation / Aerospace

Heinkel P.1079B


Single-Seat, All-Weather Heavy Fighter Proposal [ 1946 ]



The Heinkel P.1079B single-seat, all-weather fighter was the second of five designs all falling under the P.1079 project designation.



Authored By: Staff Writer | Last Edited: 09/01/2019 | Content ©www.MilitaryFactory.com | The following text is exclusive to this site.

VIEW SPECIFICATIONS [+]
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.

A subsequent P.1079B design, the so-called "P.1079C", took on many of the same qualities listed above and added heavier sweep to the mainplanes, deleted the vertical tail fin altogether, and reverted to a crew of two (in tandem, back-to-back). The same armament was retained as was the twin turbojet layout.©MilitaryFactory.com
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Specifications



Heinkel - Nazi Germany
Manufacturer(s)
Nazi Germany (abandoned)
Operators National flag of modern Germany National flag of Nazi Germany
1946
Service Year
Nazi Germany
National Origin
Cancelled
Project Status
1
Crew
0
Units


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
575 mph
(925 kph | 499 knots)
Max Speed
32,808 ft
(10,000 m | 6 miles)
Ceiling
1,647 miles
(2,650 km | 1,431 nm)
Range


MACH Regime (Sonic)
Sub
Trans
Super
Hyper
HiHyper
ReEntry
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030


PROPOSED:
4 x 30mm MK108 automatic cannons in nose section (two guns per fuselage side).


0
Hardpoints


P.1079B - Base Project Designation.


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