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SHACKLETON MR2/AEW PERFORMANCE DATA.

Power Plants

Four 12-cylinder, 60’ Vee, pressure liquid-cooled, two-speed, single-stage supercharged Rolls-Royce Griffon engines producing 1960 hp (2435 hp with water methanol) at maximum power.

Variants
 

MR2

MR2

AEW/T.2

 

Ph I/II

Ph III

57/57A

58

58

Propellers

De Havilland 13 ft-diameter counter-rotating, constant-speed, fully feathering units.

FRONT: Left-hand tractor DF 1 60/3 34/1 or DB 171/334/1 with basic setting and fine pitch 23’, feathered 90’.
REAR: Right-hand tractor DF 1 60/336/1 or DB 171/336/1 with basic setting and fine pitch 24’, feathered 91’.

Fuel System

AvGas 100/130 NATO F-13.

Tank Capacities (gallons)     

MR 2

MR2

T.2/AEW
Ph I/II/font> Ph III

 

3292

3350

3350

Dimensions

 

(Ft)

MR2

Wing span

 

120

Length

 

87.3

Height

 

17.5

Tailplane

 

33

Wheel Track

 

23.75

Weights (lb)

 

MR 2

MR2/T.2

AEW.2

 

 

Ph III

 

Empty

51,400

59,000

58,800

Loaded (normal)

84,000

89,000

89,000

Loaded (maxT/O)

86,000

95,500

96,100

Landing (normal)

72,000

80,000

80,000

Stores load (with full fuel)

6,000 approx

6,000 approx

6,000 approx

Stores load (max)

15,000

15,000

 

Speeds

 

MR 2

MR 2

AEW2

 

 

Ph III

 

Max speed @12,000 ft mph

299

286

262

Max cruise @10,000 ft mph

249

249

 

Long- range cruise                 180-200 mph depending on weight @1,500 to5,000 Ft

Landing speed mph

114

116

116

Stalling speed mph

88

92

92

Initial rate of climb (ft/mm)

920

900

900

Initial rate of climb (3 engine ft/min)

495

463

460

Ceiling (Ft)

20,200

18,800

 

Range (nm) at 5,000ft at 190 mph

1,980

1,720

 

Radius of 4 hour patrol (nm)

700

670

 

Endurance (hours) (20% reserve)

14.6

13

13

Max still air range (nm)

2,900

2,780

2,700

T/O distance (Ft) to 50Ft

 using Water Methanol

 

3,750

5,460

 

Data conversion

Imperial  
1 nautical mile (nm) = 1.136 statute miles
1 mile/hour (mph) = 0.88 knots     
1 Gallon (gals) = 7.2 lb