Lippisch P.13


Usage

Ramjet/rocket fighter

Developed by Hubert, the first version of the P 13 was a tailless high-speed bomber, with fore-and-aft tandem propellers and two piston engines.

A completely different plane, designed by Lippisch, also was called the P 13 (actually P 13a). The P 13a was designed to make use of an unusual fuel source for an airplane: coal. Liquid fuel was getting scarce, and a plane which could burn coal products would have been very desirable. 

Wind tunnel tests of the P 12 and P 13a and tests of free flight models were very successful, and did not reveal any problems.

Another version of the P 13 had a much wider wing, and used a cylindrical combustion area.

Still yet another version of the P 13 became the DM-1 full scale flight test model

 

Status

Design

Powerplant

One Lippisch coal-burning ramjet plus auxiliary rocket motor

Span

5.92 m

Length

6.70 m

Wing Area

20.0 m2

Aspect Ratio

1.75

Maximum Weight

2,295 kg

Wing loading

114.75 kg/m2

Maximum speed

1,650 km/hr at high altitude

Endurance

45 minutes with 800 kg coal

Maximum speed

 1,200 km/h @ 5,900 m

Cruising speed

 850 km/h

Armament

Two MK 103 30 mm cannon

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P 13 sketch

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Concept sketch of the P 13a

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Detail sketch of the P-13a

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Control schematic

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Layout designs leading to the DM-1

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Detail of propulsion system

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Artist's drawing of P 13 in flight

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Larger version of the P 13 with two vertical tails.

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