Terminal Kl 105
Terminal Kl 105 | |
---|---|
Type: | Sports and touring aircraft |
Design country: | |
Manufacturer: | |
First flight: |
1938 |
Number of pieces: |
11 |
The Klemm Kl 105 was a civil sport and touring aircraft from Leichtflugzeugbau Klemm GmbH .
development
The aircraft was designed in 1938 using the partial shell construction developed and patented by Hanns Klemm himself (DE 729100 of November 6, 1936). The aircraft was a cantilever low-wing aircraft in all-wood partial shell construction with an uncovered rigid normal chassis. The two-man crew sat side by side in a closed cabin. The breaking load multiple was 7.2. The engine drove a rigid two-bladed wooden propeller two meters in diameter. The outer wing parts were foldable so that the aircraft was only 2.3 meters wide for parking. Due to the war, only eleven sample machines were produced.
Technical specifications
Parameter | Terminal Kl 105 data |
---|---|
crew | 1 |
Passengers | 1 |
length | 7.35 m |
span | 10.92 m |
height | 2.0 m |
Wing area | 15.0 m² |
Wing extension | 8.0 |
Empty mass | 340 kg |
Payload | 220 kg |
Max. Takeoff mass | 560 kg |
Wing loading | 37 kg / m² |
Power load | 11 kg / hp |
Area performance | 3.3 hp / m² |
Engine | a Zündapp 9-092 with 50 PS (37 kW) or a Hirth HM 515 with 65 PS (48 kW) |
fuel | 55 l |
Top speed | 150 km / h |
Cruising speed | 135 km / h |
Landing speed | 65 km / h |
Rate of climb | 1.8 m / s near the ground |
Rise time | 12 min at 1000 m |
Service ceiling | 3000 m |
Range | 500 km |
Flight duration | 3.6 h |
literature
- Heinz J. Nowarra : The German Air Armament 1933-1945. Bernard & Graefe Verlag, Koblenz 1993, ISBN 3-7637-5464-4 .
- Günter Brinkmann, Kyrill von Gersdorff, Werner Schwipps: Sports and travel aircraft. Guidelines of diverse development. Bernard & Graefe Verlag, 1995, ISBN 978-3763761104 .
Individual evidence
- ↑ Werner von Langsdorff : Handbook of aviation . Born in 1939. 2nd, unchanged edition. J. F. Lehmann, Munich 1937, p. 456 .