| General Information |
| Type |
Anito-1, Aviavnito-1 |
| Function |
General |
| Year |
1935
|
| Crew |
1 |
| Powerplant |
| Type |
M-11
|
| Power at 0m |
100hp |
| Size |
| Length |
8.4m |
| Height |
?m |
| Wingspan |
12.6m |
| Wing area |
24m2 |
| Weights and loads |
| Empty |
815kg |
| Loaded |
1160kg |
| Wing Load (kg/m2) |
48.3 |
| Power load (kg/hp) |
11.6 |
| Speed |
| at 0m |
204km/h |
| Landing |
60km/h |
| Roll |
| Landing |
120m 14sec |
| Takeoff |
190m 15sec |
| Range |
| Practical |
666km |
| Ceiling |
| Ceiling |
5040m |
| Climb |
| 1000m |
?min |
| Payload |
| Fuel+Oil |
86+14 kg |
| Cargo |
?kg |
| Seats |
2 |
Aviavnito-1 (Anito-1) by N.K.Nurov and S.A.Elibekian
Anito-1 (Aviavnito-1) was designed for participation in the Light Safe Airplane contest, called by Osoaviakhim in 1934. Low wing monoplane with 3-seat enclosed cabin could be used for liaison, sport, tourism. Cabin floor had a hatch for parachuting people or cargo.
Fuselage - variable-thickness wooden monocoque of oval cross-section. Two-spar wing (plywood skinning) carried ailerons and large-span landing flap. Ailerons and tail controls were covered with fabric. Fixed main undercarriage was fitted with airdynamic fairings. Rubber cord shock absorbers - hidden in the fuselage.
Being of wooden design, Anito-1 was somewhat large for 100hp engine, but clean lines and high assembly quality guaranteed high performance. Strength and reliability of construction were tested in the 1935 (September 5 to 9). Aircraft participated in the circuit flight endurance contest and finished second.
| Predecessors |
Modifications |
| None |
none |
