Heli-Sport

Manufacturer:

Heli-Sport

Country:

Italy

Commercial designation:

Kompress Charlie

Technical designation:

CH-7

Version, Variant:

Charlie

Type:

Conventional

Currently produced:

Y

Typical missions:

Civil

Flight conditions:

VFR

First flight:

1996

Landing system:

skids

Blades number:

2

Tail blades number:

2

MTOW with external loads:

450 kg

992.25 lbs

MTOW with only internal loading:

450 kg

992.25 lbs

Empty weight:

275 kg

606.375 lbs

External payload:

0 kg

0 lbs

Internal payload:

205 kg

452.025 lbs

Standard fuel tank:

48 kg

105.84 lbs

with optionnal external fuel tank:

63 kg

138.915 lbs

Cruise speed:

160 km/h

86.4 kt

Maximum cruise speed:

0 km/h

0 kt

Vne:

209 km/h

112.86 kt

Max negative g @ MTOW:

0 g

Max positive g @ MTOW:

0 g

Range with normal tanks:

480 km

259.2 nm

Max range with auxiliary external tanks:

480 km

259.2 nm

Max endurance @ min consumption speed:

03:00:00 h:min

Rate of climb @ SL:

0 m/s

0 ft/min

Rate of climb @ SL @MTOW:

7.5 m/s

1476 ft/min

IGE max hovering altitude, MTOW:

3500 m

11480 ft

IGE max hovering altitude, empty:

0 m

0 ft

IGE max hovering altitude, ISA+20°C, MTOW:

0 m

0 ft

IGE max hovering altitude, ISA+20°C, empty:

0 m

0 ft

OGE max hovering altitude, MTOW:

2500 m

8200 ft

OGE max hovering altitude, empty:

0 m

0 ft

OGE max hovering altitude, ISA+20°C, MTOW:

0 m

0 ft

OGE max hovering altitude, ISA+20°C, empty:

0 m

0 ft

Service ceiling ISA, MTOW:

5000 m

16400 ft

Max operating altitude, empty weight:

0 m

0 ft

Highest use Temperature:

0 °C

0 °F

Lowest use Temperature:

0 °C

0 °F

APU in HC:

N

Engine manufacturer:

Rotax

Model:

914 Turbo

Engines quantity:

1

Powerplant category:

piston

Main rotor rotation speed:

510 rpm

Fuel consumption @ SL @ max continuous speed:

0 kg/kW/h

0 lbs/hp/h

Minimum consumption speed @ SL:

104 km/h

56.16 kt

Fuel consumption @ eco cruise speed @SL:

0 kg/h

0 lbs/h

Fuel consumption @ min consumption speed @ SL:

0 kg/h

0 lbs/h

Engines nominal power:

74 kW

100.566 hp

Transmission shaft max continuous power:

85 kW

115.515 hp

Transmission shaft max power:

85 kW

115.515 hp

Takeoff power 5 min:

85 kW

115.515 hp

OEI 30s power:

85 kW

115.515 hp

OEI 2min power:

85 kW

115.515 hp

OEI max continuous power :

85 kW

115.515 hp

OEI max continuous transmission power:

85 kW

115.515 hp

OEI 30 sec transmission power:

85 kW

115.515 hp

OEI 2 min transmission power:

85 kW

115.515 hp

Overall length:

7.05 m

23.124 ft

Rotor diameter:

6.27 m

20.5656 ft

Tail rotor diameter:

1.02 m

3.3456 ft

Fuselage length:

0 m

0 ft

Overall height:

2.35 m

7.708 ft

Main rotor blades chord:

0.18 m

0.5904 ft

Tail rotor blades chord:

9.7 m

31.816 ft

Mast tilt angle:

0 °

Noise at flyover, level:

0 dB EPNL

Noise at flyover, limit:

0 dB EPNL

Noise at takeoff, level:

0 dB EPNL

Noise at takeoff, limit:

0 dB EPNL

Noise at landing, level:

0 dB EPNL

Noise at landing, limit:

0 dB EPNL

Crew:

1

Max pax number:

1

Average price:

100000 $