Template:Aircraft specs/testcases
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Revision as of 23:07, 16 November 2014 by blackwiki>Jonesey95 (add test cases notice)
- REDIRECT Template:Testcases notice
- From a page move: This is a redirect from a page that has been moved (renamed). This page was kept as a redirect to avoid breaking links, both internal and external, that may have been made to the old page name.
Contents
One of everything
(fictional metric)
Data from source name
General characteristics
- Crew: one pilot
- Capacity: lots of passengers
- Length: 20 m (65 ft 7 in) nose probe to tail light
- Wingspan: 30 m (98 ft 5 in) with extra tips
- Height: 5 m (16 ft 5 in) to top of rudder
- Airfoil: NACA something
- Empty weight: 5,000 kg (11,023 lb) absolutely dry
- Gross weight: 7,500 kg (16,535 lb) all up
- Max takeoff weight: 7,800 kg (17,196 lb) if you must
- Fuel capacity: 1500 litres
- Extra note: something else
- Powerplant: 4 × Rolls-Whitney AS5 turbines, 5,000 kN (1,100,000 lbf) thrust each at full power dry, 1,500 kN (340,000 lbf) with afterburner
Performance
- Maximum speed: 500 km/h (310 mph, 270 kn) flat out
- Cruise speed: 350 km/h (220 mph, 190 kn) nice and gentle
- Stall speed: 160 km/h (99 mph, 86 kn) full flaps and praying
- Never exceed speed: 800 km/h (500 mph, 430 kn) on a good day
- Minimum control speed: 155 km/h (96 mph, 84 kn) whatever this means
- Range: 1,000 km (620 mi, 540 nmi) full tank
- Combat range: 500 km (310 mi, 270 nmi) travelling light
- Ferry range: 2,000 km (1,200 mi, 1,100 nmi) with extra tanks
- Service ceiling: 10,000 m (33,000 ft) half full
- Rate of climb: 10 m/s (2,000 ft/min) kind of gentle
- Fuel consumption: 22 kg/km (78 lb/mi)
(fictional imp)
but with only metric values in the params
Data from source name
General characteristics
- Crew: one pilot
- Capacity: lots of passengers
- Length: 65 ft 7 in (20 m) nose probe to tail light
- Wingspan: 98 ft 5 in (30 m) with extra tips
- Height: 16 ft 5 in (5 m) to top of rudder
- Airfoil: NACA something
- Empty weight: 11,023 lb (5,000 kg) absolutely dry
- Gross weight: 16,535 lb (7,500 kg) all up
- Max takeoff weight: 17,196 lb (7,800 kg) if you must
- Fuel capacity: 1500 litres
- Extra note: something else
- Powerplant: 4 × Rolls-Whitney AS5 turbines, 1,100,000 lbf (5,000 kN) thrust each at full power
Performance
- Maximum speed: 310 mph (500 km/h, 270 kn) flat out
- Cruise speed: 220 mph (350 km/h, 190 kn) nice and gentle
- Stall speed: 99 mph (160 km/h, 86 kn) full flaps and praying
- Never exceed speed: 500 mph (800 km/h, 430 kn) on a good day
- Minimum control speed: 96 mph (155 km/h, 84 kn) whatever this means
- Range: 620 mi (1,000 km, 540 nmi) full tank
- Service ceiling: 33,000 ft (10,000 m)
- Rate of climb: 2,000 ft/min (10 m/s) kind of gentle
- Fuel consumption: 78 lb/mi (22 kg/km)
(fictional in knots)
but only metric in params
Data from source name
General characteristics
- Crew: one pilot
- Capacity: lots of passengers
- Length: 65 ft 7 in (20 m) nose probe to tail light
- Wingspan: 98 ft 5 in (30 m) with extra tips
- Height: 16 ft 5 in (5 m) to top of rudder
- Airfoil: NACA something
- Empty weight: 11,023 lb (5,000 kg) absolutely dry
- Gross weight: 16,535 lb (7,500 kg) all up
- Max takeoff weight: 17,196 lb (7,800 kg) if you must
- Fuel capacity: 1500 litres
- Extra note: something else
- Powerplant: 4 × Rolls-Whitney AS5 turbines, 1,100,000 lbf (5,000 kN) thrust each at full power
Performance
- Maximum speed: 270 kn (310 mph, 500 km/h) flat out
- Cruise speed: 190 kn (220 mph, 350 km/h) nice and gentle
- Stall speed: 86 kn (99 mph, 160 km/h) full flaps and praying
- Never exceed speed: 430 kn (500 mph, 800 km/h) on a good day
- Minimum control speed: 84 kn (96 mph, 155 km/h) whatever this means
- Range: 540 nmi (620 mi, 1,000 km) full tank
- Service ceiling: 33,000 ft (10,000 m)
- Rate of climb: 2,000 ft/min (10 m/s) kind of gentle
- Fuel consumption: 23 lb/mi (22 kg/km)
- Something else: but nothing special
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)
- Height: 22 ft 2 in (6.76 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