History

Germany's fortunes in World War II (1939-1945) began to take a turn in 1943 and did not worsen until 1944, prompting the Luftwaffe authorities to seek solutions to avoid defeat. The main enemy of the day was a relentless day and night Allied air bombardment campaign that took a toll on German infrastructure and wartime capabilities.

Focused on turbojet technology, German engineers from various wartime aerospace companies set out to design various war-winning aircraftif they could ever lift off.

Project "P. 1092" as a design study focused on a reusable compact jet fighter/interceptor platform focused on simplifying production, maintenance and training.

The project eventually included a few related offshoots, none of which were actually built during the war - but still gave us a glimpse into where the company was thinking about its turbojet fighter.

P. 1092 item from its original form "P. 1092A" to successive quotes "P. 1092/1", "P. 1092/2" and "P. 1092/3" using the features defined by the original A model drawings Further development or less.

In the first iteration of the P. 1092A, the aircraft had a ventral-mounted air intake to take in a single turbojet engine buried in the lower fuselage. The nose was used to accommodate the weapons (side-by-side automatic cannons), and the single-seat cockpit was located behind the cannon and above the engine. As the engine is drawn under the nose, the engine exits through an opening integrated under the empennage, which ends up in front of the actual empennage.

The tail tapers back in the usual fashion and is given a "V-Plane" arrangement. The wing main aircraft is mounted centrally on both sides of the fuselage, with swept back on both the leading and trailing edges. The landing gear consists of a fairly modern retractable wheeled tricycle arrangement.

In this work came the subsequent P. 1092/1, which simplified the original A-type concept, added a dorsal ridge, revised engine housing, relocated front wheels (now behind the air intakes, while not before). and traditional single tail. The main feature of this model should be the variable "wing sweep" main aircraft function, which can be changed during flight depending on the current flight phase (takeoff, landing, cruise, fast flight).

The successor P. 1092/2 took the same design and added a deeper hull to it. Overall, many aspects of the original have been retained, including the single-seat layout, traditional rear wing and suspended turbojet fuselage.

The third iteration of the series became P. 1092/3 of July 1943 - the focus of this article - and was a major departure from the norm by moving the cockpit further aft, in front of the rear wing, and fully integrated to the bottom of the caudal fin. This shifts the pilot's position to the rear of the boat, but does so to improve high-speed efficiency by reducing drag.

Of course, this comes at a cost - that is, from the cockpit pilot's point of view, it causes take-off and landing hazards. The retractable tricycle landing gear was taken from template P. 1092/2, as was the low ground clearance.

Despite the drawbacks of the rear pilot placement, the proposed changes free up the front of the fuselage to accommodate larger caliber weapon systems, while still allowing the fighter to maintain its relatively compact size. As a result, armament would be increased to 4 x 30mm MK108 autocannons, mounted in pairs on either nose, for a powerful single-shot kill against any Allied bomber of the time.

Another feature revised in the P. 1092/3 design study is the air intakes - now bifurcated (split) to improve airflow for single-engine mounts. Power comes from a single Junkers Jumo 004C series turbojet engine, which will produce 2,237 pounds of thrust.

The low position of the turbojet should facilitate maintenance, repair and replacement, and refueling, and reduce the number of airflow ducts.

As designed, the improved fighter should have an overall length of 26.5 feet, a wingspan of 30.8 feet, and a height of 11.8 feet. No other specifications were estimated/completed until the end of the war in Europe in May 1945.

In any case, the P. 1092/3 ended its era only as a "paper plane", one of many such aircraft maintained by the German aviation agency and Luftwaffe authorities before Germany's eventual defeat. It existed only as a design study at the time and was used for comparison with other proposals at the time.

In addition to the three iterations of the P. 1092, there were also the twin-engine P. 1092/4 (with the cockpit above the nose) and the P. 1092/5 version, the latter more in line with the P. 1092/. 3 design - Again, none of them progress past the drawing board or concept stage.

Specification

Basic

Year:
1945
Status:
Cancel
Staff:
1

Production

[0 units]:
Messerschmitt - Nazi Germany

Roles

- Fighter

- Intercept

- X-Plane / Development

Dimensions

Length:

26.57 ft (8.1 m)

Width:

9.4m

Height:

3.6m

Weight

Curb Weight:

2,630 kg

MTOW:

3,670 kg

(difference: +2,293 pt)

Performance

1 x Junkers Jumo 004C turbojet with 2,237 pounds of thrust.

Performance

Maximum Speed:

590 mph (950 km/h; 513 knots)

Service Limit:

36,745 ft (11,200 m; 6.96 mi)

Maximum range:

559 miles (900 km; 486 nautical miles)

Rate of climb:

1,103 m/min (3,620 ft/min)

Armor

Suggestions:

4 x 30mm MK108 automatic cannons mounted in the nose assembly.

Changes

p. 1092/3 - Basic project title; design study only.

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