.jpg "ARCHON SF-1 Ultralight aircraft. First flight: 2009")
In numbers Through the lens Video
This greek design ultralight airplane was developed by Mr. G. Iliopulos. It's a single-seater, single-engine high-wing full-metal airplane, with possible small scale use of composite materials. The tricycle undercarriage is not retractable, with one wheel on each leg. It is equipped with a 46 hp thrust engine. The fuels are located in tanks in the wings with a total capacity of 56 lt. The cabin has one seat and the single-piece cover opens upwards.
ARCHON SF-1 It can carry alternative engines, like the Rotax 503 or 532 or 582.
It first flight in June 2009 and received a flight certificate from the Italian authorities under the number I-A281.
Three-view drawing
Technical specifications
|
DESIGNER
|
G-Aerosports |
|---|---|
|
COUNTRY
|
Greece |
|
TYPE
|
Ultralight aircraft |
|
CREW
|
1 |
|
POWER-PLANT
|
One engine, single-propeller |
| Power, h.p. | 1x50 until 130 (specifications based on 65 h.p. engine). |
|
DIMENSIONS
|
|
|
Length, m
|
8,00
|
|
Height, m
|
2,25
|
|
Wing span, m
|
7,25
|
|
Wing area m2
|
-
|
| Propeller diameter (max), m | 1,55 |
| WEIGHT | |
| Maximum take-off, kg | 322,5 |
| Normal take-off, kg | - |
| Empty aircraft, kg | 200 |
| Internal fuel, l | 80 |
| Payload, kg | - |
| PERFORMANCE | |
| Maximum permitted speed, km/h | 250 |
|
Cruising speed, km/h
|
200
|
|
Maneuvering speed, km/h
|
160
|
|
Maximum speed with extended camber flaps, km/h
|
130
|
|
Maximum overload, g
|
+6 / -3
|
|
Rate of climb, m/min
|
- |
| Service ceiling, m | - |
| Take-off distance, m |
150
|
|
Range, km
|
- |
| ARMAMENT | Doesn't have (defensive). |