A002
IRKUT A-002
IRKUT A-002
Aircraft
Name
A-002
Manufacturer
Wing
Rotary
Position
Two-blade main rotor
Tail
Regular tail, mid set
WTC
L
Type Code
G1P
Engine
Piston
Engine Count
Single
Position
Above cabin
Landing gear
Tricycle fixed
Manufactured as
IRKUT A-002
A002
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 (metric)
9.80 m
Length (metric)
4.98 m
Height (metric)
3.17 m
Powerplant
1 x AviaSmart B-H4K flat-four cylinder piston with fluid cooling; digital control unit
Indicative Performance Data
Take-Off
V2
n/a
Distance
0 m
MTOW
800 kg
Initial Climb (to 5000 ft)
IAS
n/a
ROC
500 ft/min
Initial Climb (to FL150)
IAS
n/a
ROC
n/a
Initial Climb (to FL240)
IAS
n/a
ROC
n/a
MACH Climb
MACH
n/a
ROC
n/a
Cruise
TAS
113 kts
MACH
n/a
Ceiling
100
Range
270 NM
Initial Descent (to FL240)
MACH
n/a
ROD
n/a
Descent (to FL100)
IAS
n/a
ROD
n/a
Descent (FL100 & below)
IAS
n/a
MCS
n/a
ROD
n/a
Approach
Vapp (IAS)
n/a
Distance
0 m
