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IRKUT A-002

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A002
Aircraft
Name A-002
Manufacturer IRKUT
Wing Rotary
Position Two-blade main rotor
Tail Regular tail, mid set
WTC Light
Type code G1P
Engine Piston
Engine count Single
Position Above cabin
Landing gear Tricycle fixed
Mass group 1


Manufacturered as:

IRKUT A-002


IRKUT A-002

IRKUT A-002 IRKUT A-002 3D

Description

The Irkut A-002 is a three seat, pusher configuration autogyro developed in Russia through the 2000s by the United Constructor Bureau for Light Aircraft team of the Irkutsk Aircraft Production Association (IAPO) "Irkut" as the first independent product. The take-off from a place is possible when speed of a wind exceeds 8 m/s, otherwise running start up to 15 m is necessary.

Technical Data

Wing span 9.80 m32.152 ft
Length 4.98 m16.339 ft
Height 3.17 m10.4 ft
Powerplant 1 x AviaSmart B-H4K flat-four cylinder piston with fluid cooling; digital control unit
Engine model

Performance Data

Take-Off Initial Climb
(to 5000 ft)
Initial Climb
(to FL150)
Initial Climb
(to FL240)
MACH Climb Cruise Initial Descent
(to FL240)
Descent
(to FL100)
Descent (FL100
& below)
Approach
V2 (IAS) kts IAS kts IAS kts IAS kts MACH TAS 113 kts MACH IAS kts IAS kts Vapp (IAS) kts
Distance 0 m ROC 500 ft/min ROC ft/min ROC ft/min ROC ft/min MACH ROD ft/min ROD ft/min MCS kts Distance 0 m
MTOW 800800 kg
0.8 tonnes
kg
Ceiling FL100 ROD ft/min APC
WTC L Range 270270 nm
500,040 m
500.04 km
1,640,551.182 ft
NM

Accidents & Serious Incidents involving A002

None on SKYbrary {{#semantic-title:Name}}