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Resposta to "Chegaram os Russos - Perdas russas durante a operação militar na Síria"

A-10 Thunderbolt II versus Sukhoi Su-25 Frogfoot

 

CATEGORY

Su-25 Frogfoot

A-10 Thunderbolt II

Unit cost in USD millions

13-15

20-25

Fuel economy in km/l

0,39

0,31

Fuel economy in NM/g

0,90

0,72

Fuel tank capacity in litres

3500

4850

Fuel tank capacity in gallon

924

1280

Range on internal fuel in km

1350

1500

Range on internal fuel in miles

837

930

Range on internal fuel in NM

729

810

Powerplant/Engines

2 × Tumansky R-195

2 × General Electric TF34-GE-100A

Dry thrust in kN

2 x 44

2 x 40

Dry thrust in lbf

2 x 9500

2 x 9000

Afterburner in kN

NO

NO

Afterburner in lbf

NO

NO

Max. Speed in Mach

0,77

0,70

Max. Speed in km/h

943

858

Max. Speed in mph

586

533

Minimal thrust/weight ratio

0,40

0,21

Normal thrust/weight ratio

0,61

0,36

Maximal thrust/weight ratio

0,80

0,58

Overall length in meters

15,36

16,26

Overall length in ft

50,38

53,33

Wingspan in meters

14,36

17,53

Wingspan in ft

47,10

57,50

Height in meters

4,80

4,47

Height in ft

15,74

14,66

Wing area in sq meters

31,00

47,00

Wing area in sq ft

333,56

505,72

Empty weight in kg

10700

11300

Empty weight in lb

23540

24860

Maximal take-off weight in kg

21500

23000

Maximal take-off weight in lb

47300

50600

Minimal wing-loading in kg/m2

345

297

Normal wing-loading in kg/m2

555

482

Maximal wing-loading in kg/m2

691

599

Rate of climb in m/sec

65

30

Rate of climb in ft/min

12799

5907

First flight

1975

1972

 

- See more at: http://www.kamov.net/versus/a-...sthash.3LMEeAqo.dpuf

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