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An Open Access Journal

Table 11 Aircrat data sheet

From: A new aircraft architecture based on the ACHEON Coanda effect nozzle: flight model and energy evaluation

Geometric data

Wing span

m

13.45

Ft

44.2

Length

m

11.09

Ft

36.5

Height

m

3.49

Ft

11.6

Wing Area

m2

21

Sq ft

225.8

Aerodynamic constants

CD

–

0.026

  

E

–

0.85

  

CLmax

–

2.27

  

Weights

Empty weight

kg

1845

Lb

4,069

Useful load

kg

1262

Lb

2,783

kg

662

lb

1459.46

Max takeoff weight

kg

3107

Lb

6,850

Max on board fuel

kg

640

Gal

213

Batteries (Boston Power Swing® 5300 Rechargeable Lithium-ion Cell)

kg

1550

Wh/kg

170

Ah

4,420

Propulsion

Engine

Two 240 kW (325 hp) turbocharged and fuel injected TSIO-520-VBs

Four Plettemberg Nov. 15 mounted in two ACHEON Nozzle

Power

kW

240

Hp

325

kW

150

hp

203

Weght

kg

219.5

Lb

484

kg

11.5

lb

25.4

Performances

Max speed

m/s

118.9

Kts

230

Max cruising speed

m/s

109.4

Kts

213

Stall Speed

m/s

46.3

Kts

71.4

Stall Speed Carrriage

m/s

25.1

Kts

48.9

Initial rate of climb

m/s

7.366

ft/min

1,450

Service ceiling

m

8200

Ft

26,900

Long range cruising speed

m/s

84.4

Kts

164

To be calculated

Range with reserves at economical cruising speed

km

2360

Nm

1273

To be calculated