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«INDELA SKY LAB» flying laboratory makes it possible to carry out flight tests of all types of aircraft nods and blocks in the following directions:
- flight tests to evaluate aerodynamic, strength, vibroacoustic and operation characteristics at all flight stages, including critical modes;
- flight tests with regard to development of algorithms of software and equipment of on-board control complexes;
- flight tests of systems on prevention of critical flight modes;
Such unique flight characteristics of «INDELA SKY LAB» unmanned helicopter as: possibility to hover, perform vertical takeoff and landing and to perform mechanical translations in any direction have from the very beginning resulted in the idea of utilizing the helicopter as an aircraft test bed.
Characteristics
Engine four-cycle, two-cylinder, water-cooled
Takeoff power kW 20.2
Fuel consumption l/h 6
Key geometric characteristics
Length with main rotor mm 3754
Length Nose to Tail mm 3052
Main rotor diameter mm 3168
Height mm 1346
Wheelbase mm 1180
Weight data
Maximum takeoff weight kg 125
Useful load kg 25
Fuel-carrying capacity l 10
Basic flight characteristics
Maximum speed horizontal level flight km/h 70
Static ceiling m 1000
Maximal vertical speed m/s 1.5
Flight duration (height 100-500 m) h 5
Wind (takeoff and landing) m/s up to 7
Available power
Payload Electrical power W 150@12V DC