Вертолет Торнадо TH-34, Київ

TORNADO TH-34
Standard specification

LIGHT HELICOPTER

eng: MOTSU EJ253
Located in Ukraine. Kharkov. We can train, send, collect anywhere in the world

Airworthiness certification for experimental or ultralight requirements.
• Empty weight - 400 kg;
• Payload 350 kg;
• Crew 1 person + 1 (2) passenger;
• Ceiling 4000 meters;
• Weather limits 50 meters cloud cover x 500 visibility.

Also can enter the ultralight class up to 600 kg:
• Pilots 160 kg + 30 kg gasoline for 1 hour.
Based on: 400 + 160 + 30 = 590 kg

TORNADO TH-34

Basic flight performance
Flight characteristics
All flight characteristics are given for a helicopter take-off weight of 600 kg

Maximum flight speed not exceeded 200 km / h
Cruising speed135 - 140 km / h
Static hovering ceiling 2000 m
Service ceiling 4000 m
Maximum rate of climb at sea level 12 m / s
Descent speed when gliding in autorotation mode Vсн 90-100 km / h
Minimum vertical rate of descent when gliding
in autorotation mode 6.5 m / s
Maximum vertical rate of descent when gliding
in autorotation mode 10 m / s
Maximum flight duration at H = 0 . 500 m
taking into account 10% of air navigation fuel reserve 5.5 hours
Maximum flight range, taking into account 10%
aeronautical fuel reserve 590 km
Operating overload range 0.0 ... + 2.5

Estimated masses

Maximum takeoff weight 600 (800) kg
Maximum payload mass (including pilot and fuel) 300kg
Empty helicopter weight 398 kg

The mass of the crew and equipment of the helicopter:
- crew (2 people) 150 kg
- not generated fuel residue 1.0 kg
- engine oil 4.5 kg
- coolant 10 kg