Gen 4 co axial
ultralight helicopter
pictures, Gen 4 co axial helicopter images, Gen 4 helicopter photographs, Lightsport Aircraft Pilot
newsmagazine aircraft directory.
|
Lightsport
Aircraft Pilot is a directory of aircraft that generally fit
into what are described as ultralight aircraft, advanced ultralight
aircraft,
light sport aircraft, experimental light sport aircraft, experimental
aircraft, amateur built aircraft, ELSA or homebuilt
aircraft in the United States and Canada. These include
weight shift aircraft, more commonly known as trikes,
powered parachutes, and powered para-gliders.
|
|
|
|
|
|
Gen 4 Helicopter Pictures, images of the
Gen 4 co axial helicopter ultralight, experimental, lightsport aircraft.
|
|
|
|
To view the
pictures, images of the Gen 4 co axial helicopter click on the smaller
images and they will enlarge. To return to the index page for the
the Gen 4 co axial helicopter click on Gen 4 Helicopter Index link, to view
video of the Gen 4 co axial helicopter click on the Video link, to
return to the Main Index click on the Lightsport Aircraft
Pilot link. |
|
|
|
|
|
|
Gen 4 co axial helicopter ultralight -
experimental lightsport aircraft |
|
 |
|
GEN 4 Ultralight
Helicopter Specifications |
|
Type |
Two-stroke,
air-cooled, 125cc, horizontally opposed.
Two-cylinder.
|
|
Output
power |
10 hp per engine (40
hp with four)
|
|
Weight |
6.2 lb per engine
|
|
RPM |
7,000 to 8,000 rpm in
normal flight
|
|
Ignition |
CDI
|
|
Fuel |
30:1 mixture of
automobile gasoline and two stroke oil
|
|
Engine
TBO |
500 hr
|
| |
Rotors |
|
Diameter |
4.0m (13'1")
|
|
RPM |
800-900 rpm |
|
Pitch |
Fixed (ground
adjustable)
|
|
Transmission |
CFRP composite
|
|
Gear |
Integral reduction
gear and counter-rotating system
|
| |
Flight
Controls |
|
Roll &
pitch |
By the
control bar (which travels the whole rotor head |
|
Yaw |
Left hand (through an
electric controlled differential gear)
|
|
Altitude |
Right
hand (throttle lever; operated with the right thumb) |
| |
|
|
Empty weight |
70 kg (155 lb)
|
|
Max
takeoff weight |
220 kg (485 lb)
|
|
Endurance |
30 to 60 min.
(Depending on payload)
|
|
Cruising speed |
100 km/h (60 mph)
|
|
Ceiling |
3,000m (10,000 ft)
(estimate) |
|
VNE |
200
km/h (120 mph) |
Engineering System CO. Ltd.
5652-83 SASAGA, MATSUMOTO-shi,
NAGANO-ken, JAPAN 399-0033
TEL:
+81(263)26-1212 FAX: +81(263)26-1213
|
|
|
|
|
|
To view larger images of the Gen 4 co axial helicopter ultralight -
experimental lightsport aircraft click on the smaller image. |
|
|
|
|
|
|
Light Sport Aircraft Pilot News Web Magazine.
You may link to these pages or print
them out for your own personal use.
No part of this
publication may be copied or distributed, transmitted, transcribed,
stored in a retrieval system, or translated into any human or computer
language, in any form or by any means, electronic, mechanical,
manual, or otherwise, without the written permission of Light Sport
Aircraft Pilot News.
By copying or paraphrasing the intellectual
property on this site, you're automatically signing a binding contract
and agreeing to be billed $10,000 payable immediately. Copyright Light Sport Aircraft
Pilot News. Email
|
|
