Messerschmitt (Lippisch) Me 334

History

Alexander Lippisch was a renowned aeronautical engineer during Nazi Germany, known for designing rocket-powered aircraft and tailless research planes. His most significant achievement was the Me 163 "Komet," a rocket-powered interceptor produced by Messerschmitt for the Luftwaffe during World War II. Lippisch also worked on other projects like the "P.13," "P.15," and "P.20," which were jet-powered aircraft with evolving designs.

After the war, Lippisch contributed to the development of the Dornier Aerodyne VTOL test bed. He also designed the Messerschmitt Me 334, a piston-powered aircraft with a propeller arrangement, intended as an insurance policy in case the production of the Me 163B V1 rocket-powered aircraft faced delays. The Me 334 featured a wingspan of 30.5 feet, a length of 22.9 feet, and a height of 12 feet. It was armed with two 13mm MG131 machine guns for offensive capabilities and was powered by a Daimler-Benz DB605A-C 12-cylinder engine producing 1,475 horsepower, driving a three-bladed propeller.

However, the successful development of the Me 163B's rocket motor made the Me 334 obsolete, leading to its abandonment in 1943. Despite his innovative designs, Lippisch's work on the Me 334 did not progress beyond the concept stage due to changing circumstances during the war.

Specification

Basics

Year of Service: 1943

Origins: Nazi Germany

Status: Cancel

Crew: 1

Production: 0

Manufacturer: Messerschmitt (Lippisch) - Nazi Germany

Roles

Air-to-air combat, fighter

The general ability to actively attack other aircraft of similar form and function, usually using guns, missiles and/or airborne missiles.

Intercept

The ability to intercept incoming airborne threats with high performance, usually speed and rate of climb.

X-Plane (development, prototype, tech demo)

Aircraft designed for prototyping, technology demonstration, or research/data collection.

Notable Features

Armor

Armor assigned to protect the pilot/crew compartment and/or critical operating systems enhances survivability.

Fader support

The design features a rearward push rod arrangement in contrast to the more traditional pull rod arrangement.

Wing sweep

The main plane or leading edge has retraction lines for improved high-speed performance and handling.

High-speed performance

Can accelerate to higher speeds than the average aircraft at the time.

Rescue process

A manual process to allow the pilot and/or crew to exit in the event of an onboard emergency.

Depression in crew members

Support the pressurization required for crew survival at higher operating altitudes.

Closed crew room

There are partially or fully enclosed crew work areas.

Scalable

Has retractable/retractable landing gear to maintain aerodynamic efficiency.

Dimensions and Weight

Length: 23. 0 feet (7.00m)

Width/span: 30.5 feet (9.30m)

Height: 12. 2 feet (3.72m)

Cured weight: 5,071 lbs (2,300 kg)

MTOW: 6,614 lbs (3,000 kg)

Wgt Difference: +1,543 lbs (+700 kg)

Main aircraft structure

Monoplane

Designed to use a single main wing main aircraft; this is the most popular arrangement of main aircraft.

Central Install

The main aircraft is mounted below the center on the sides of the fuselage.

Swipe back

The floor plan features a swept wing along the leading edge of the main aircraft, promoting higher operating speeds.

Performance

Installed: 1 x Daimler-Benz DB605A-C 12-cylinder inverted-V liquid-cooled piston engine in a thrust arrangement to drive a three-bladed propeller unit at the rear of the fuselage.

Maximum speed: 326 km/h (525 km/h | 283 kn)

Cruising speed: 370 km/h (595 km/h | 321 kn)

Maximum speed difference: +-43 km/h (+-70 km/h | -38 knots)

Area: 1,243 km (2,000 km | 3,704 nautical miles)

Rate of climb: 4,000 ft/min (1,219 m/min)

Weapons

Proposed: 2 x 13mm MG131 Heavy Machine Guns (HMG), one shot at each wing root.