Difference between revisions of "Template:Aircraft specs/testcases"
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blackwiki>GraemeLeggett (→(fictional in knots): add extra performance) |
blackwiki>GraemeLeggett (→One of everything: add more numbers and notes) |
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|power original= | |power original= | ||
|thrust original= | |thrust original= | ||
| − | |eng1 kn-ab=<!-- afterburners --> | + | |eng1 kn-ab=1500<!-- afterburners --> |
|eng1 lbf-ab=<!-- afterburners --> | |eng1 lbf-ab=<!-- afterburners --> | ||
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|range nmi= | |range nmi= | ||
|range note=full tank | |range note=full tank | ||
| − | |combat range km= | + | |combat range km=500 |
|combat range miles= | |combat range miles= | ||
|combat range nmi= | |combat range nmi= | ||
| − | |combat range note= | + | |combat range note=travelling light |
| − | |ferry range km= | + | |ferry range km=2000 |
|ferry range miles= | |ferry range miles= | ||
|ferry range nmi= | |ferry range nmi= | ||
| − | |ferry range note= | + | |ferry range note=with extra tanks |
|endurance=<!-- if range unknown --> | |endurance=<!-- if range unknown --> | ||
|ceiling m=10000 | |ceiling m=10000 | ||
|ceiling ft= | |ceiling ft= | ||
| − | |ceiling note= | + | |ceiling note=half full |
|g limits=<!-- aerobatic --> | |g limits=<!-- aerobatic --> | ||
|roll rate=<!-- aerobatic --> | |roll rate=<!-- aerobatic --> | ||
Revision as of 21:53, 3 September 2014
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)
- 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