Template:Aircraft specs/testcases

One of everything

(fictional metric)

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{{Aircraft specs/sandbox}}

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)

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

Side by side comparison

{{Aircraft specs}}

{{Aircraft specs/sandbox}}

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)

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

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{{Aircraft specs/sandbox}}

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

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)

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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)

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

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Data from British Civil Aircraft 1919-72 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) Airfoil: modified RAF31 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)

Data from British Civil Aircraft 1919-72 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) Airfoil: modified RAF31 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)

prop testing section

no number value test

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General characteristics Propellers: 1 m (3 ft 3 in) diameter Performance	General characteristics Propellers: 1 m (3 ft 3 in) diameter Performance

diameter test

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General characteristics Performance	General characteristics Performance

type test

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General characteristics Propellers: 2.4 m (7 ft 10 in) diameter Performance	General characteristics Propellers: 2.4 m (7 ft 10 in) diameter Performance

type test

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General characteristics Propellers: Rotol reversing propeller Performance	General characteristics Propellers: Rotol reversing propeller Performance

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General characteristics Propellers: 317-bladed Rotol reversing propeller Performance	General characteristics Propellers: 317-bladed Rotol reversing propeller Performance

Rotodyne

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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) Disk loading: 5.2 lb/sq ft (25 kg/m2) Power/mass (prop): 0.17 hp/lb (0.28 kW/kg)

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) Disk loading: 5.2 lb/sq ft (25 kg/m2) Power/mass (prop): 0.17 hp/lb (0.28 kW/kg)

Embedded lists with extra information

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Data from astronautix.com General characteristics Crew: One Length: 16 ft 5 in (5 m) Wingspan: 16 ft 5 in (5 m) Diameter: 5 ft 0 in (1.52 m) Wing area: 160 sq ft (15 m2) Empty weight: 2,646 lb (1,200 kg) Gross weight: 7,937 lb (3,600 kg) Aspect Ratio: 1.6 Powerplant: 1 × SpaceDev N2O/HTPB hybrid rocket, 16,500 lbf (73.5 kN) thrust Isp: 250 s (4.2 min) Burn time: 80 seconds Performance Maximum speed: Mach 3.09 (2370 mph, 3815 kph) Range: 40 mi (65 km, 35 nmi) Service ceiling: 367,000 ft (112,000 m) Rate of climb: 82,000 ft/min (420 m/s) Wing loading: 49 lb/sq ft (240 kg/m2) Thrust/weight: 2.08

Data from astronautix.com General characteristics Crew: One Length: 16 ft 5 in (5 m) Wingspan: 16 ft 5 in (5 m) Diameter: 5 ft 0 in (1.52 m) Wing area: 160 sq ft (15 m2) Empty weight: 2,646 lb (1,200 kg) Gross weight: 7,937 lb (3,600 kg) Aspect Ratio: 1.6 Powerplant: 1 × SpaceDev N2O/HTPB hybrid rocket, 16,500 lbf (73.5 kN) thrust Isp: 250 s (4.2 min) Burn time: 80 seconds Performance Maximum speed: Mach 3.09 (2370 mph, 3815 kph) Range: 40 mi (65 km, 35 nmi) Service ceiling: 367,000 ft (112,000 m) Rate of climb: 82,000 ft/min (420 m/s) Wing loading: 49 lb/sq ft (240 kg/m2) Thrust/weight: 2.08

Swept parm

{{Aircraft specs|genhide=Y |prime units?=met |span m=20}}

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Wingspan: 20 m (65 ft 7 in) Performance	Wingspan: 20 m (65 ft 7 in) Performance

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{{Aircraft specs|genhide=Y |prime units?=met |span m=20 |swept m=12}}

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Wingspan: 20 m (65 ft 7 in) Swept wingspan: 12 m (39 ft 4 in) swept Performance	Wingspan: 20 m (65 ft 7 in) Swept wingspan: 12 m (39 ft 4 in) swept Performance

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{{Aircraft specs|genhide=Y |lower span m=20 |prime units?=met |upper span m=15}}

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Upper wingspan: 15 m (49 ft 3 in) Lower wingspan: 20 m (65 ft 7 in) Performance	Upper wingspan: 15 m (49 ft 3 in) Lower wingspan: 20 m (65 ft 7 in) Performance

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{{Aircraft specs|genhide=Y |lower span m=20 |prime units?=met |swept m=12 |upper span m=15}}

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Upper wingspan: 15 m (49 ft 3 in) Lower wingspan: 20 m (65 ft 7 in) spread, 12 m (39 ft 4 in) swept Performance	Upper wingspan: 15 m (49 ft 3 in) Lower wingspan: 20 m (65 ft 7 in) spread, 12 m (39 ft 4 in) swept Performance