Fregata J6
As the motor glider "Fregata J6" belongs to the safest aircrafts in aviation, which results from the Lift-to-drag ratio up to 24 (28 with single wheel ver.) Authorizations to fly are widely available, for all range of pilots, from the youngest to the oldest generation. As a single-seat design is the most optimal in terms of economic use (low weight, size and fuel consumption). Composite airframe structure enabled the implementation of combining the characteristics of an aircraft and a glider.Purpose:
Engines:
“J & AS Aero – Design” was established in 1991 by Polish famous aviation constructor Mr. Jarosław Janowski Based on Mr. Janowski’s first motor glider project in 1965, company started designing and testing new motor glider “Fregata J6”.
In 2002 company introduced to the market an Aircraft dedicated for commercial use.
In 2003 “ J & AS Aero – Design” signed the contract with British BAE Systems for supplying 50 motor gliders (UAV/RPA - remotely piloted aircraft) built in HERTI program („High Endurance Rapid Technology Insertion”), project was completed in 2010.
In 2011 Aero Design started recreational project “Fregata J6” for US market customer and “Fregata J6” for commercial use (pipe lines, borders, electrical lines, national parks patrol Aircraft) Both Aircrafts were finally built in 2012 and tested in 2013/2014. That year Aero – Design introduced to the markets a unique motor glider “Fregata J6” and started designing works on New Tandem “Fregata J7”.
Professional & Outstanding ideas of our passionate team makes us unique in every sense.
In 2003 “ J & AS Aero – Design” signed the contract with British BAE Systems for supplying 50 motor gliders (UAV/RPA - remotely piloted aircraft) built in HERTI program („High Endurance Rapid Technology Insertion”), project was completed in 2010.
NAME | VALUE |
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Wing span | 12,55 m |
Lenght | 5,11 m |
High | 1,58 m |
Lift area | 9,13 m² |
Aspect ratio | 17,25 |
Wing loading | 43,8 kG/m² |
Main aerodynamic chord | 0,762 m |
Distance between reference chord and hull’s chord | 0,038 m |
Dihedral angle | 1.5° |
Wing swept angle | 0° |
Surface of empennage | 1.48 m² |
Empennage span | 2.96 m |
Angle between wings’ half | 105° |
WEIGHTS DATA: | VALUE |
---|---|
Basic empty mass | 292,4 kG |
Maximum payload | 147,6 kG |
Minimum wing mass | 102,5 kG |
Maximum mass in flight |
440,0 kG |
DOWNLOAD DOCUMENTATION: | |
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Service Manual Fregata J6 |
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Service Manual Aerohonda_BF50D |
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Pilot Operating handbook FregataJ6 |
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