| Picture |
|
| Manufacturer |
Jen C Ellehammer
|
| Type |
Coaxial Helicopter with Cyclic Control
|
| Introduced |
9/28/1912
|
| In production? |
No
|
| Units produced |
1
|
| Price US $ |
0.00
|
| Overall Length |
0 ft
|
| Length |
0 ft
|
| Height |
0 ft
|
| Width |
0 ft
|
| |
|
| |
|
| Description |
A co-axial design by Ellehammer (Denmark) with cyclic pitch control, this machine made several hops but couldn't achieve controlled free-flight. It was destroyed in a crash in 1916.
|
| Advertisement |
|
| Design features |
- Lower rotor disk covered with fabric in order to serve as a parachute in case of a fatal failure
- Cyclic pitch mechanism
- Movable pilot seat for additional kineshetic control
- Tracktor propeller mounted to the airfrane for forward propulsion
|
|
A co-axial design by Ellehammer (Denmark) with cyclic pitch control, this machine made several hops but couldn't achieve controlled free-flight. It was destroyed in a crash in 1916.
|
|
- Advertisement -
|
Design features:
- Lower rotor disk covered with fabric in order to serve as a parachute in case of a fatal failure
- Cyclic pitch mechanism
- Movable pilot seat for additional kineshetic control
- Tracktor propeller mounted to the airfrane for forward propulsion
|
| Persons |
1
|
| Max. Range |
0 mi
|
| Cruise Speed |
0 mph
|
| Max. Speed |
0 mph
|
| Max. rate of Climb |
0 ft/min
|
| HOGE ceiling |
0 ft
|
| Service Ceiling |
0 ft
|
| Gross Weight |
0 lb
|
| Empty Weigt |
0 lb
|
| Useful Load |
0 lb
|
| Fuel Capacity |
0 gallons
|
| Number of Engines |
1
|
| Engine Type |
Piston
|
| Engine Code |
|
| Horse Power |
36
|
| Rotorhead |
Coaxial
|
| Number of rotorblades |
6
|
| Rotor Diameter |
24.5 ft
|
| Number of tail rotorblades |
0
|
| Tailrotor Diameter |
0 ft
|
|