Miloch
January 1st 20, 03:37 PM
https://en.wikipedia.org/wiki/Messerschmitt_M_17
The M 17 was a German single-engine high-wing sports monoplane. It was designed
by Willy Messerschmitt in 1925 in Bamberg. This aircraft won many competitions
and allowed Willy Messerschmitt to build his first factory.
The design of the M 17 could be traced back via the powered S 16 and S 15
aircraft to the Messerschmitt-Hirth S 14 glider. The aircraft was a two-seater
almost completely made of wood and weighed only 198 kg (437 lb). The engine was
a 22 kW (29 hp) Bristol Cherub II. The pilot had no forward visibility.
In September 1926, pilot Eberhard von Conta, and the writer Werner von
Langsdorff flew in an M 17 from Bamberg to Rome. This marked the first time the
central Alps were crossed with a light aircraft. The flight lasted more than 14
hours and they had to refuel every three hours, since the tank could hold only
28 L (7 US gal). They reached an altitude of 4,500 m (14,760 ft).
Role
Sports plane
National origin
Germany
Manufacturer
Flugzeugbau Messerschmitt Bamberg
Designer
Willy Messerschmitt
First flight
January 1925
Introduction
1925
Primary user
Germany
Number built
8
Only one of the six-eight machines built survived and is today in the Deutsches
Museum in Munich.
A replica was built by the Messerschmitt Foundation (first flight April 14,
2004) and makes regular appearances at the International Aerospace Exhibition in
Berlin. It weighs 40 kg (90 lb) more than the original due to additional
equipment (radio and rescue system) and is now at the Manching Aviation Museum
in Ingolstadt, Bavaria.
Specifications
Crew: 2
Length: 5.85 m (19 ft 2 in)
Wingspan: 11.6 m (38 ft 1 in)
Height: 1.5 m (4 ft 11 in)
Wing area: 10.4 m2 (112 sq ft)
Airfoil: Göttingen 535
Empty weight: 186 kg (410 lb)
Max takeoff weight: 370 kg (816 lb)
Fuel capacity: 28 l (7.4 US gal; 6.2 imp gal)
Powerplant: 1 × Bristol Cherub II 2-cylinder air-cooled horizontally-opposed
piston engine, 22 kW (29 hp)
Propellers: 2-bladed fixed-pitch propeller
Performance
Maximum speed: 140 km/h (87 mph, 76 kn)
Cruise speed: 125 km/h (78 mph, 67 kn)
Stall speed: 65 km/h (40 mph, 35 kn)
Range: 600 km (370 mi, 320 nmi)
Service ceiling: 4,000 m (13,000 ft)
*
The M 17 was a German single-engine high-wing sports monoplane. It was designed
by Willy Messerschmitt in 1925 in Bamberg. This aircraft won many competitions
and allowed Willy Messerschmitt to build his first factory.
The design of the M 17 could be traced back via the powered S 16 and S 15
aircraft to the Messerschmitt-Hirth S 14 glider. The aircraft was a two-seater
almost completely made of wood and weighed only 198 kg (437 lb). The engine was
a 22 kW (29 hp) Bristol Cherub II. The pilot had no forward visibility.
In September 1926, pilot Eberhard von Conta, and the writer Werner von
Langsdorff flew in an M 17 from Bamberg to Rome. This marked the first time the
central Alps were crossed with a light aircraft. The flight lasted more than 14
hours and they had to refuel every three hours, since the tank could hold only
28 L (7 US gal). They reached an altitude of 4,500 m (14,760 ft).
Role
Sports plane
National origin
Germany
Manufacturer
Flugzeugbau Messerschmitt Bamberg
Designer
Willy Messerschmitt
First flight
January 1925
Introduction
1925
Primary user
Germany
Number built
8
Only one of the six-eight machines built survived and is today in the Deutsches
Museum in Munich.
A replica was built by the Messerschmitt Foundation (first flight April 14,
2004) and makes regular appearances at the International Aerospace Exhibition in
Berlin. It weighs 40 kg (90 lb) more than the original due to additional
equipment (radio and rescue system) and is now at the Manching Aviation Museum
in Ingolstadt, Bavaria.
Specifications
Crew: 2
Length: 5.85 m (19 ft 2 in)
Wingspan: 11.6 m (38 ft 1 in)
Height: 1.5 m (4 ft 11 in)
Wing area: 10.4 m2 (112 sq ft)
Airfoil: Göttingen 535
Empty weight: 186 kg (410 lb)
Max takeoff weight: 370 kg (816 lb)
Fuel capacity: 28 l (7.4 US gal; 6.2 imp gal)
Powerplant: 1 × Bristol Cherub II 2-cylinder air-cooled horizontally-opposed
piston engine, 22 kW (29 hp)
Propellers: 2-bladed fixed-pitch propeller
Performance
Maximum speed: 140 km/h (87 mph, 76 kn)
Cruise speed: 125 km/h (78 mph, 67 kn)
Stall speed: 65 km/h (40 mph, 35 kn)
Range: 600 km (370 mi, 320 nmi)
Service ceiling: 4,000 m (13,000 ft)
*