| Picture |
|
| Manufacturer |
Aeris Naviter
|
| Type |
AN-2
|
| Introduced |
1/1/2011
|
| In production? |
Yes
|
| Units produced |
0
|
| Price US $ |
130,000.00
|
| Overall Length |
0 ft
|
| Length |
17.3 ft
|
| Height |
11.3 ft
|
| Width |
2.6 ft
|
| |
|
| |
|
| Description |
Aeris Naviter develops rotor dynamic technologies and is a provider of aeronautical services in a mostly B2B market. One of the company’s developments is the AN-2 two-seater tandem helicopter. A prototype was on show at the Paris Air Show in June 2009. This coaxial helicopter is targeted at both the experimental kit-build helicopter market and as a ready-to-fly machine under the European VLR class of certified helicopters.
At the time of writing (2013), the machine is not certified, while the kit-build version is likewise unavailable. There is also no indication that the prototype has ever been flown
|
| Advertisement |
|
| Design features |
- Tricycle landing gear
- Aluminum sheet fuselage
- Two seater tandem configuration
- Tailboom with H-tail
|
Aeris Naviter develops rotor dynamic technologies and is a provider of aeronautical services in a mostly B2B market. One of the company’s developments is the AN-2 two-seater tandem helicopter. A prototype was on show at the Paris Air Show in June 2009. This coaxial helicopter is targeted at both the experimental kit-build helicopter market and as a ready-to-fly machine under the European VLR class of certified helicopters.
At the time of writing (2013), the machine is not certified, while the kit-build version is likewise unavailable. There is also no indication that the prototype has ever been flown
|
|
- Advertisement -
|
Design features:
- Tricycle landing gear
- Aluminum sheet fuselage
- Two seater tandem configuration
- Tailboom with H-tail
|
| Persons |
2
|
| Max. Range |
466 mi
|
| Cruise Speed |
93 mph
|
| Max. Speed |
105 mph
|
| Max. rate of Climb |
0 ft/min
|
| HOGE ceiling |
0 ft
|
| Service Ceiling |
15000 ft
|
| Gross Weight |
1320 lb
|
| Empty Weigt |
860 lb
|
| Useful Load |
460 lb
|
| Fuel Capacity |
0 gallons
|
| Number of Engines |
1
|
| Engine Type |
Piston
|
| Engine Code |
Lycoming IO 233 LSA
|
| Horse Power |
115
|
| Rotorhead |
Fully articulated coaxial
|
| Number of rotorblades |
4
|
| Rotor Diameter |
22.9 ft
|
| Number of tail rotorblades |
0
|
| Tailrotor Diameter |
0 ft
|
|