Arado Ar 77
Arado Ar 77 | |
---|---|
Type: | Trainer aircraft |
Design country: | |
Manufacturer: | |
First flight: |
December 10, 1934 |
Commissioning: |
- |
Production time: |
1933-1935 |
Number of pieces: |
2 |
The low wing Arado Ar 77 was built by the Arado aircraft factory. It was supposed to be used as a training aircraft and for bombing exercises, but did not go into series production in favor of the Fw 58 .
Technical specifications
Manufacturer: | Arado aircraft works |
Type: | Ar 77 |
Design: | Low-wing aircraft |
Design type: | self-supporting |
Usage: | Feeder airliner, training on |
2-engine machines, in sparks and bombs | |
Engines: | 2 Argus As 10 C, 2 × 240 HP = 480 HP |
Crew: | 2 pilots, 1 radio operator, 1 teacher |
Special features: | Double steering |
Parameter | Data |
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Dimensions: | |
span | 19.20 m |
Length, gr. | 12.50 m |
Height, gr. | 3.20 m |
Wheel track | 3.70 m |
Type of tire | High performance tires |
wheel size | 690 × 200 |
Star wheel size | 290 × 110 |
Wheel brake | Yes |
Contents of the fuel tank | 340 l |
Contents of the lubricant reservoir | 25 l |
Area: | |
Wing with ailerons | 50.50 m² |
Aileron, total | 5.73 m² |
Flaps, total | 4.26 m² |
Tailplane | 9.60 m² |
Vertical stabilizer | 4.09 m² |
Wing: | |
outline | trapezoidal |
Arrow shape | 10 ° |
V shape | 5 ° |
Root depth | 3.60 m |
average Area depth | 2.60 m |
Wing extension | 7.30 |
Breaking load multiple | 7th |
Masses: | |
Empty mass | 1930 kg |
Payload | 1010 kg |
Takeoff mass | 2940 kg |
Propeller: | |
design type | Rigid propeller |
drive | directly |
diameter | 2.30 m |
Number of sheets | 2 |
Building material | Wood |
Sense of rotation | right |
Helical surface | 2 x 4.16 = 8.32 m² |
Building materials: | |
Structure | Wooden frame, covered with fabric above / plywood planked below |
Fuselage | Tubular steel frame, fabric-covered |
Tail unit | Metal frame, covered with fabric |
Services: | |
Flight duration | 3.6 h |
Range | 720 km |
Fuel consumption | 59.0 l / 100 km |
Top speed | 240 km / h |
Marching speed | 200 km / h |
Landing speed | 84 km / h |
Service ceiling with 2 engines | 5000 m |
Summit height with 1 motor | 1800 m |
Ascent times at 1000 m | 3.5 min |
Wing loading | 57.20 kg / m² |
Power load | 6.02 kg / hp |
Area performance | 9.51 hp / m² |
Helical area performance | 57.70 hp / m² |