Messerschmitt Me P.1092/2

History

With the advent of turbojets during World War II (1939-1945), German engineers were looking for a suitable compact, single-seat, single-engine, high-altitude fighter to take advantage of their newfound performance. For Messerschmitt, one of those paths led to the "P. 1092A" project, a series of related fighter studies aimed at providing solutions.

The original main aircraft had slightly swept wings, short, retractable tricycle landing gear, and had its dual-gun armament concentrated on the nose. Some unique qualities are a bottom turbojet casing (at the belly line of the fuselage) and a "V-tail" aircraft layout.

This version appeared in May 1943.

The successor "P. 1092.1" retained many of these characteristics, but began to be streamlined, with a more contoured nose and a deeper fuselage. In addition, a more traditional single-tail fin is now used (an arrangement not unlike that of the yet-to-be-present Me 262 fighter).

The next step in the series is "P. 1092/2", which is the focus of this article. While the plane maintains its original layout, the fuselage is gradually lowered, with a raised spine visible behind the cockpit. The nose is more rounded and the armament of the 2 x 30mm MK103 autocannons is extended by 2 x 15mm MG151/15 autocannons - the cannons are mounted in pairs on either side of the front hull (two on one side). ). The landing gear is still in a tricycle arrangement, close to the center of the boat, while the wing main aircraft on the outboard section, borrowed from the Me 262 fighter, performs recoil mainly on the leading edge.

A main aircraft with an "extended wing" with an elongated tip to improve long-range performance was also considered.

Power comes from a single Junkers Jumo 004C turbojet engine, providing up to 2,240 pounds of thrust, which hangs below the fuselage, is drawn in through an air intake under the nose cone, and depleted under the tail boom. Estimated performance specs include a top speed of nearly 580 mph, a range of up to 540 miles and a ceiling of up to 36,750 feet.

The central location of the powerful turbojet will give the fighter an excellent rate of climb. For the proposed "extended-wing" main aircraft, the same design is believed to be slightly slower (567 mph) but farther (602 mph), and could operate at a higher altitude (39,700 ft) to engage the enemy head-on Bomber formation.

In any event, the promising P. 1092/2 was not selected for additional design/development work and continues to serve the company, primarily for comparative analysis in future studies, while providing important lessons for engineers .

Specification

Basic

Production

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Performance

Performance

Armor

Changes