fs26 Moseppl | |
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| |
Role | Motor glider |
National origin | West Germany |
Manufacturer | Akaflieg Stuttgart |
First flight | 25 September 1970 |
Number built | 1 |
The Akaflieg Stuttgart fs26 Moseppl is a German single-seat motor glider with twin fins and rudders designed and built by Akaflieg Stuttgart. [1] First flown on the 25 September 1970 it was designed as an experiment and not intended for production. [1]
The fs26 Moseppl is a cantilever high-wing monoplane with a monocoque nacelle fuselage and a glassfibre/balsa sandwich wing structure, fitted with airbrakes but no flaps or ailerons. [1] To make room for the engine the Moseppl has twin fins and rudders attached to the wing trailing edge with an all-moving tailplane between the tops of the vertically surfaces. [1] The pilot sits in an enclosed cockpit with a transparent canopy and the landing gear is a retracting rear monowheel and non-steerable nosewheel. [1] The rear-mounted engine is a 26 hp (19 kW) Solo-Hirth engine with a variable pitch pusher propeller. [1]
Data from Jane's All the World's Aircraft 1973-74. [1]
General characteristics
Performance
Related lists
fs26 Moseppl | |
---|---|
| |
Role | Motor glider |
National origin | West Germany |
Manufacturer | Akaflieg Stuttgart |
First flight | 25 September 1970 |
Number built | 1 |
The Akaflieg Stuttgart fs26 Moseppl is a German single-seat motor glider with twin fins and rudders designed and built by Akaflieg Stuttgart. [1] First flown on the 25 September 1970 it was designed as an experiment and not intended for production. [1]
The fs26 Moseppl is a cantilever high-wing monoplane with a monocoque nacelle fuselage and a glassfibre/balsa sandwich wing structure, fitted with airbrakes but no flaps or ailerons. [1] To make room for the engine the Moseppl has twin fins and rudders attached to the wing trailing edge with an all-moving tailplane between the tops of the vertically surfaces. [1] The pilot sits in an enclosed cockpit with a transparent canopy and the landing gear is a retracting rear monowheel and non-steerable nosewheel. [1] The rear-mounted engine is a 26 hp (19 kW) Solo-Hirth engine with a variable pitch pusher propeller. [1]
Data from Jane's All the World's Aircraft 1973-74. [1]
General characteristics
Performance
Related lists