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Revision as of 12:26, 21 October 2009 by blackwiki>GraemeLeggett (→Specifications (Fairey Rotodyne "Y"): both switch)
Contents
Specifications (Fairey Rotodyne "Y")
General characteristics
- Crew: 2
- Capacity: 48 passengers
- Length: 58 ft 8 in (17.9 m)
- Wingspan: 90 ft 0 in (27.4 m)
- Height: 22 ft 2 in (6.76 m)
- Wing area: 6,360 ft² (591 m²)
- Loaded weight: 33,000 lb (15,000 kg)
- Max. takeoff weight: 38,000 lb (17,000 kg)
- Powerplant:
- 4 × rotor tip jet burning compressed air/fuel, () each
- 2 × Napier Eland turboprops, 2,800 hp (2,100 kW) each
Performance
- Maximum speed: 213 mph (343 km/h)
- Range: 520 mi (830 km)
- Wing loading: 5.2 lb/ft² (25 kg/m²)
- Power/mass (prop): 0.17 hp/lb (280 W/kg)
Specifications (Tarrant Tabor estimated)
Data from The British Bomber since 1914[1]
General characteristics
- Crew: Six
- Length: 73 ft 2 in (22.31 m)
- Wingspan: 131 ft 3 in (40.02 m)
- Height: 37 ft 3 in (11.36 m)
- Wing area: 4,950 ft² (460 m²)
- Empty weight: 24,750 lb (11,250 kg)
- Loaded weight: 44,672 lb (20,305 kg)
- Powerplant: 6 × Napier Lion 12 cylinder, water cooled broad arrow engines (four tractor, two pusher), 450 hp (336 kW) each
Performance
- Maximum speed: over 96 knots (110 mph, 177 km/h)
- Endurance: 12 hours
- Service ceiling: 13,000 ft (3,970 m)
- Wing loading: 9.02 lb/ft² (44.1 kg/m²)
- Power/mass: 0.06 hp/lb (0.099 kW/kg)
- Climb to 10,000 ft (3,050 m): 33 min 30 sec
Armament
- Bombs: approximately 4,600 lb planned
Specifications (Göppingen Gö 4 )
General characteristics
- Crew: Two, pilot and instructor
- Length: 6.74 m (22 ft 1 in)
- Wingspan: 14.8 m (48 ft 7 in)
- Height: dunno ()
- Empty weight: 180 kg (400 lb)
Performance
- sink rate: 1.0 m/s (200 ft/min)
Specifications (R101)
Data from not given
General characteristics
- Crew: 45
- Capacity: 100 passengers
- Length: 777 ft (237 m)
- Wingspan: ()
- Height: ()
- Powerplant: 5 × Beardmore Tornado 8 cylinder Diesel, 585 hp (436 kW) each
Performance
- Maximum speed: 71 mpg (114 km/h)
Stuff
- ↑ Mason, Francis K (1994). The British Bomber since 1914. London: Putnam Aeronautical Books. pp. 126–127. ISBN 0 85177 861 5.