- 2T Tornado 280 engine with 32 HP
- electrically operated flaps
- brakes on main wheels
- steerable front wheel
- cockpit ventilation
- fuel tank 18 l
- speedometer, altimeter, variometer
- engine parameter monitor
- flap position indicator
- fuel gauge
A one-person motor glider designed for recreational flying
KR-010 Elf
FUSELAGE - shell structure, made of two assemblies; tail boom integral with the vertical stabilizer and the main cockpit part of the fuselage permanently connected to each other.
COCKPIT - one-piece cockpit canopy that opens to the side, equipped with handles and locks, in the open position it is supported on a string.
Ergonomic interior enabling easy use also for larger Pilots. The pilot's seat is adjusted by using the appropriate thickness of the seat and backrest.
WING - bipartite, equipped with slotted flaperons and optionally with aerodynamic brakes. Proven and effective, contamination-resistant NN-1817 wing profile commonly used in glider structures Of the Warsaw University of Technology (Politechnika Warszawska), such as PW5, PW6, AOS71.
TAIL-PLANE - in the classic arrangement. UNDERCARRIAGE - fixed, tricycle with a front wheel. The resilient main landing gear leg is made of composite. The front wheel is controlled thanks to a system of levers and pushrods on the pedals, allowing a 15 degree turn to each side.
Airframe control systems:
AILERONS - applied along the entire span except for the elliptical tips of the wing. The joystick movements are transmitted to the ailerons through a rigid tappet - lever system.
FLAPS - controlled by buttons on the joystick.The drive is realized by a rigid system of tappets, torsion tubes and levers translating the energy of the electric actuator's movement into the flap deflection. The range of deflections is from -6º to + 15º, with the -6º value being the neutral position in in the trailing edge plane.
ELEVATOR - joystick movements are transferred to the elevator by a rigid tappet-lever system.
RUDDER - the movements of the pedals are transmitted to the rudder by a cable-lever system, moreover, there is a coupling with the wheel of the front landing gear.
DATA
wingspan | 10,73 m | ||
bearing surface | 10,5 m2 | ||
length | 5,45 m | ||
height | 208 cm | ||
empty weight | 120 kg | ||
maximum weight (with GRS) | 250 kg | ||
take-off weight | 250 kg | ||
cruising speed | 128 km/h | ||
maximum speed | 142 km/h | ||
stall speed | 55 km/h | ||
climb speed | 3,9 m/s | ||
take-off run | 100 m | ||
landing run | 50 m |
ROTAX 912 UL
engine power | 80 KM |
fuel tank capacity | 86 l |
fuel consumption | 10 l/h |
wingspan | 10,58 m |
bearing surface | 10,1 m2 |
length | 5,95 m |
height | 2,3 m |
empty weight (with GRS) | 305 kg |
maximum weight (with GRS) | 472,5 kg |
LSA take-off weight (with GRS) | 472,5 kg (LSA 560 kg) |
cruising speed | 189 km/h |
maximum speed horizontal flight | 210 km/h |
Vne speed | 240 km/h |
stall speed | 65 km/h |
climb speed | 6 m/s |
take-off run | 80 m |
landing run | 100 m |