Function Fuel Type




Дата канвертавання22.04.2016
Памер26.63 Kb.
Lippisch Li P.01-111



Function

Fuel Type

Fuel Cap

Fuel Cons

Load

Wt. Empty

Wt. Max

Crew

Maintenance

Fighter

AvGas

2100

2800/700

6kg

2200kg

4270kg

1

6

Minimum Takeoff

Minimum Landing

Runway Type

Trolly,500m

600m

paved

Power plant(s)

Horsepower

Turbojet engine




Length

Wingspan

Height

Speed max

Speed Cruise

Speed Stall

Tr. Move.

CM

Ceiling

Range

6.6m

7.5m

3.2m

780km/h

500km/h

140km/h

2000

78

4200m

1500km

Armaments

Ammo

Location

2 x MG 151/20 20mm cannon

2 x 120

Wing roots




























Weapon

ROF

Damage

Penetration

Magazine

Range





































History: This was the first project under the P.01 series, and was designed shortly after Lippisch arrived at the Messerschmitt A.G. It was part of the Project X design period, which was the code name given the Me 163 project, and is dated November 20, 1939.
          The Lippisch P.01-111 had a short fuselage, which included an air intake in the nose of the aircraft. It fed an unnamed turbojet engine located in the rear of the fuselage. The wings were swept back at approximately 24 degrees, and were very wide and of a short span. A single fin and rudder was mounted on the rear of the fuselage, and landing was accomplished on a retractable landing skid and tail skid. The single pilot sat in an unpressurized cockpit. Armament was to consist of two MG 151/20 20mm cannon, located in the wing roots on either side of the cockpit. This project did not evolve past the early design stage, as it was merely one of many projects designed as the Me 163 was becoming a reality.


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