With the K 10 Rudolf Kaiser brought together the desires of the contest pilots for an all-moving (pendulum) elevator, thought to have a little less drag, and the improved flight performance of the Ka 6 B-S modifications.
Because of the need to pay more attention to flying the aircraft, caused by the pendulum elevator, the K 10 was not popular. Finally, Rudolf Kaiser made pilots happy with the subsequent K 6 E, which led to a great success with this aircraft.
Technical Data
| Muster / Type | K 10 |
| Klasse / Class | Einsitzer / Single seater |
| Erstflug / Maiden flight | Juli 1963 |
| Herstellungszeitraum / Production period | 1963 – 1965 |
| Stückzahl / Number of pieces | 12 |
| Konstrukteuer / Designer | Rudolf Kaiser |
| Spannweite / Span | 15 m |
| Rumpflänge / Fuselage length | 6.64 m |
| Höhe / Height | 1.65 m |
| Flügelfläche / Wing area | 12.53 m² |
| Flügelstreckung / Wing aspect ratio | 17.96 |
| Flügelprofil / Airfoil | FX 40 mod. – FX 30 mod. |
| Leermasse / Empty weight | 210 kg |
| Höchstflugmasse / Max. weight | 320 kg |
| Max. Flächenbelastung / Max. wing load | 25.5 kg/m² |
| Geringstes Sinken / Min. sink | 0.7 m/s |
| Gleitzahl / Best glide ratio | 32 |
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