Template:Aircraft specs/testcases
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Revision as of 08:25, 23 September 2013 by blackwiki>JurgenNL (File renamed: File:Rotodyne.png → File:Fairey Rotodyne three-view silhouette.png File renaming criterion #1: Uploader requested.More detailed, less generic name)
Contents
Testing auto reversing (MET, no inches)
General characteristics
- Length: 2 m (6 ft 7 in)
- Wingspan: 0.61 m (2 ft)
- Upper wingspan: 0.61 m (2 ft)
- Mid wingspan: 0.61 m (2 ft)
- Lower wingspan: 0.61 m (2 ft) spread, 0.61 m (2 ft) swept
- Diameter: 0.61 m (2 ft)
- Width: 0.61 m (2 ft)
- Height: 0.61 m (2 ft)
- Wing area: 0.19 m2 (2 sq ft) spread, 0.19 m2 (2 sq ft) swept
- Volume: 0.057 m3 (2 cu ft)
- Empty weight: 1 kg (2 lb)
- Gross weight: 1 kg (2 lb)
- Max takeoff weight: 1 kg (2 lb)
- Useful lift: 0.91 kg (2 lb)
- Powerplant: 1 × x y, 1.5 kW (2 hp) dry, 0.0089 kN (2 lbf) with afterburner
- Powerplant: 2 × v f, 1.5 kW (2 hp) each dry, 0.0089 kN (2 lbf) with afterburner
- Powerplant: 3 × f g, 1.5 kW (2 hp) each dry, 0.0089 kN (2 lbf) with afterburner
- Main rotor diameter: 3× 0.61 m (2 ft)
- Main rotor area: 0.19 m2 (2 sq ft)
- Propellers: 2-bladed sds, 0.61 m (2 ft) diameter
Performance
- Maximum speed: 3.2 km/h (2.0 mph, 1.7 kn)
- Cruise speed: 3.2 km/h (2.0 mph, 1.7 kn)
- Stall speed: 3.2 km/h (2.0 mph, 1.7 kn)
- Never exceed speed: 3.2 km/h (2.0 mph, 1.7 kn)
- Minimum control speed: 3.2 km/h (2.0 mph, 1.7 kn)
- Range: 3.2 km (2.0 mi, 1.7 nmi)
- Combat range: 3.2 km (2.0 mi, 1.7 nmi)
- Ferry range: 3.2 km (2.0 mi, 1.7 nmi)
- Service ceiling: 0.61 m (2 ft)
- Rate of climb: 0.010 m/s (2 ft/min)
- Rate of sink: 0.010 m/s (2 ft/min)
- Wing loading: 9.8 kg/m2 (2 lb/sq ft)
- Disk loading: 9.8 kg/m2 (2 lb/sq ft)
- Fuel consumption: 0.56 kg/km (2 lb/mi)
Specifications
Data from British Civil Aircraft 1919-72[1]
General characteristics
- Crew: 2
- Length: 4.0 m (22 ft 3.5 in)
- Wingspan: 7.0 m (27 ft 4 in) overall
- Upper wingspan: 6.0 m (22 ft 0 in)
- Lower wingspan: 8.33 m (27 ft 4 in)
- Wing area: 5.0 m2 (164 sq ft) [2]
- Airfoil: modified RAF31[3]
- Empty weight: 200 kg (480 lb)
- Gross weight: 400 kg (874 lb)
- Powerplant: 1 × Bristol Cherub III flat twin piston engine
- Propellers: 2 m (6 ft 7 in) diameter
Performance
- Maximum speed: 105 km/h (65 mph, 56 kn) [3]
prop testing section
no number value test
General characteristics
- Propellers: 1 m (3 ft 3 in) diameter
Performance
diameter test
General characteristics Performance
type test
General characteristics
- Propellers: 2.4 m (7 ft 10 in) diameter
Performance
Rotodyne display test
Rotodyne - aircraft specifications template
General characteristics
- Crew: 2
- Capacity: 48 passengers
Performance
Rotodyne - this template
General characteristics
- Crew: 2
- Capacity: 48 passengers
- Length: 58 ft 8 in (17.88 m)
- Wingspan: 90 ft (27 m)
- Wing area: 6,360 sq ft (591 m2)
- Gross weight: 33,000 lb (14,969 kg)
- Max takeoff weight: 38,000 lb (17,237 kg)
- Powerplant: 4 × rotor tip jet burning compressed air/fuel
- Powerplant: 2 × Napier Eland turboprop, 2,800 hp (2,100 kW) each
- Main rotor diameter: 90 ft (27 m)
Performance
- Maximum speed: 213 mph (343 km/h, 185 kn)
- Range: 520 mi (840 km, 450 nmi)
- Wing loading: 5.2 lb/sq ft (25 kg/m2)power mass 0.17