Difference between revisions of "Template:Aircraft specs/testcases"
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blackwiki>GraemeLeggett (→top: an example) |
blackwiki>GraemeLeggett (→One of everything (metric): add imp and knots first examples) |
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| − | ==One of everything (metric)== | + | ==One of everything== |
| + | === (fictional metric)=== | ||
{{Aircraft specs | {{Aircraft specs | ||
|ref=<!-- reference -->source name | |ref=<!-- reference -->source name | ||
|prime units?=met<!-- imp or kts first for US aircraft, and UK aircraft pre-metrification, | |prime units?=met<!-- imp or kts first for US aircraft, and UK aircraft pre-metrification, | ||
| + | met(ric) first for all others. You MUST choose a format, or no specifications will show --> | ||
| + | <!-- | ||
| + | General characteristics | ||
| + | --> | ||
| + | |genhide= | ||
| + | |||
| + | |crew=one pilot | ||
| + | |capacity=lots of passengers | ||
| + | |length m=20 | ||
| + | |length ft= | ||
| + | |length in= | ||
| + | |length note=nose probe to tail light | ||
| + | |span m=30 | ||
| + | |span ft= | ||
| + | |span in= | ||
| + | |span note=with extra tips | ||
| + | |upper span m= | ||
| + | |upper span ft= | ||
| + | |upper span in= | ||
| + | |upper span note= | ||
| + | |mid span m= | ||
| + | |mid span ft= | ||
| + | |mid span in= | ||
| + | |mid span note= | ||
| + | |lower span m= | ||
| + | |lower span ft= | ||
| + | |lower span in= | ||
| + | |lower span note= | ||
| + | |swept m=<!-- swing-wings --> | ||
| + | |swept ft=<!-- swing-wings --> | ||
| + | |swept in=<!-- swing-wings --> | ||
| + | |swept note= | ||
| + | |dia m=<!-- airships etc --> | ||
| + | |dia ft=<!-- airships etc --> | ||
| + | |dia in=<!-- airships etc --> | ||
| + | |dia note= | ||
| + | |width m=<!-- if applicable --> | ||
| + | |width ft=<!-- if applicable --> | ||
| + | |width in=<!-- if applicable --> | ||
| + | |width note= | ||
| + | |height m=5 | ||
| + | |height ft= | ||
| + | |height in= | ||
| + | |height note=to top of rudder | ||
| + | |wing area sqm= | ||
| + | |wing area sqft= | ||
| + | |wing area note= | ||
| + | |swept area sqm=<!-- swing-wings --> | ||
| + | |swept area sqft=<!-- swing-wings --> | ||
| + | |swept area note= | ||
| + | |volume m3=<!-- lighter-than-air --> | ||
| + | |volume ft3=<!-- lighter-than-air --> | ||
| + | |volume note= | ||
| + | |aspect ratio=<!-- sailplanes --> | ||
| + | |airfoil=NACA something | ||
| + | |empty weight kg=5000 | ||
| + | |empty weight lb= | ||
| + | |empty weight note=absolutely dry | ||
| + | |gross weight kg=7500 | ||
| + | |gross weight lb= | ||
| + | |gross weight note=all up | ||
| + | |max takeoff weight kg=7800 | ||
| + | |max takeoff weight lb= | ||
| + | |max takeoff weight note=if you must | ||
| + | |fuel capacity=1500 litres | ||
| + | |lift kg=<!-- lighter-than-air --> | ||
| + | |lift lb=<!-- lighter-than-air --> | ||
| + | |lift note= | ||
| + | |more general= | ||
| + | *'''Extra note:''' something else | ||
| + | <!-- | ||
| + | Powerplant | ||
| + | --> | ||
| + | |eng1 number=4 | ||
| + | |eng1 name=Rolls-Whitney AS5 | ||
| + | |eng1 type=turbines | ||
| + | |eng1 kw=<!-- prop engines --> | ||
| + | |eng1 hp=<!-- prop engines --> | ||
| + | |eng1 shp=<!-- prop engines --> | ||
| + | |eng1 kn=5000<!-- jet/rocket engines --> | ||
| + | |eng1 lbf=<!-- jet/rocket engines --> | ||
| + | |eng1 note=at full power | ||
| + | |power original= | ||
| + | |thrust original= | ||
| + | |eng1 kn-ab=<!-- afterburners --> | ||
| + | |eng1 lbf-ab=<!-- afterburners --> | ||
| + | |||
| + | |eng2 number= | ||
| + | |eng2 name= | ||
| + | |eng2 type= | ||
| + | |eng2 kw=<!-- prop engines --> | ||
| + | |eng2 hp=<!-- prop engines --> | ||
| + | |eng2 shp=<!-- prop engines --> | ||
| + | |eng2 kn=<!-- jet/rocket engines --> | ||
| + | |eng2 lbf=<!-- jet/rocket engines --> | ||
| + | |eng2 note= | ||
| + | |eng2 kn-ab=<!-- afterburners --> | ||
| + | |eng2 lbf-ab=<!-- afterburners --> | ||
| + | |||
| + | |eng3 number= | ||
| + | |eng3 name= | ||
| + | |eng3 type= | ||
| + | |eng3 kw=<!-- prop engines --> | ||
| + | |eng3 hp=<!-- prop engines --> | ||
| + | |eng3 shp=<!-- prop engines --> | ||
| + | |eng3 kn=<!-- jet/rocket engines --> | ||
| + | |eng3 lbf=<!-- jet/rocket engines --> | ||
| + | |eng3 note= | ||
| + | |eng3 kn-ab=<!-- afterburners --> | ||
| + | |eng3 lbf-ab=<!-- afterburners --> | ||
| + | |more power= | ||
| + | |||
| + | |prop blade number=<!-- propeller aircraft --> | ||
| + | |prop name= | ||
| + | |prop dia m=<!-- propeller aircraft --> | ||
| + | |prop dia ft=<!-- propeller aircraft --> | ||
| + | |prop dia in=<!-- propeller aircraft --> | ||
| + | |prop dia note= | ||
| + | |||
| + | |rot number=<!-- helicopters --> | ||
| + | |rot dia m=<!-- helicopters --> | ||
| + | |rot dia ft=<!-- helicopters --> | ||
| + | |rot dia in=<!-- helicopters --> | ||
| + | |rot area sqm=<!-- helicopters --> | ||
| + | |rot area sqft=<!-- helicopters --> | ||
| + | |rot area note= | ||
| + | <!-- | ||
| + | Performance | ||
| + | --> | ||
| + | |perfhide= | ||
| + | |||
| + | |max speed kmh=500 | ||
| + | |max speed mph= | ||
| + | |max speed kts= | ||
| + | |max speed note=flat out | ||
| + | |max speed mach=<!-- supersonic aircraft --> | ||
| + | |cruise speed kmh=350 | ||
| + | |cruise speed mph= | ||
| + | |cruise speed kts= | ||
| + | |cruise speed note=nice and gentle | ||
| + | |stall speed kmh=160 | ||
| + | |stall speed mph= | ||
| + | |stall speed kts= | ||
| + | |stall speed note=full flaps and praying | ||
| + | |never exceed speed kmh=800 | ||
| + | |never exceed speed mph= | ||
| + | |never exceed speed kts= | ||
| + | |never exceed speed note=on a good day | ||
| + | |minimum control speed kmh=155 | ||
| + | |minimum control speed mph= | ||
| + | |minimum control speed kts= | ||
| + | |minimum control speed note=whatever this means | ||
| + | |range km=1000 | ||
| + | |range miles= | ||
| + | |range nmi= | ||
| + | |range note=full tank | ||
| + | |combat range km= | ||
| + | |combat range miles= | ||
| + | |combat range nmi= | ||
| + | |combat range note= | ||
| + | |ferry range km= | ||
| + | |ferry range miles= | ||
| + | |ferry range nmi= | ||
| + | |ferry range note= | ||
| + | |endurance=<!-- if range unknown --> | ||
| + | |ceiling m=10000 | ||
| + | |ceiling ft= | ||
| + | |ceiling note= | ||
| + | |g limits=<!-- aerobatic --> | ||
| + | |roll rate=<!-- aerobatic --> | ||
| + | |glide ratio=<!-- sailplanes --> | ||
| + | |climb rate ms=10 | ||
| + | |climb rate ftmin= | ||
| + | |climb rate note=kind of gentle | ||
| + | |time to altitude= | ||
| + | |sink rate ms=<!-- sailplanes --> | ||
| + | |sink rate ftmin=<!-- sailplanes --> | ||
| + | |sink rate note= | ||
| + | |lift to drag= | ||
| + | |wing loading kg/m2= | ||
| + | |wing loading lb/sqft= | ||
| + | |wing loading note= | ||
| + | |disk loading kg/m2= | ||
| + | |disk loading lb/sqft= | ||
| + | |disk loading note= | ||
| + | |fuel consumption kg/km=22 | ||
| + | |fuel consumption lb/mi= | ||
| + | |power/mass= | ||
| + | |thrust/weight= | ||
| + | |||
| + | |more performance= | ||
| + | <!-- | ||
| + | Armament | ||
| + | --> | ||
| + | |armament=<!-- add bulletted list here or if you want to use the following | ||
| + | specific parameters, remove this parameter--> | ||
| + | |guns= | ||
| + | |bombs= | ||
| + | |rockets= | ||
| + | |missiles= | ||
| + | |hardpoints= | ||
| + | |hardpoint capacity= | ||
| + | |hardpoint rockets= | ||
| + | |hardpoint missiles= | ||
| + | |hardpoint bombs= | ||
| + | |hardpoint other= | ||
| + | |||
| + | |avionics= | ||
| + | }} | ||
| + | === (fictional imp)=== | ||
| + | but with only metric values in the params | ||
| + | {{Aircraft specs | ||
| + | |ref=<!-- reference -->source name | ||
| + | |prime units?=imp<!-- imp or kts first for US aircraft, and UK aircraft pre-metrification, | ||
| + | met(ric) first for all others. You MUST choose a format, or no specifications will show --> | ||
| + | <!-- | ||
| + | General characteristics | ||
| + | --> | ||
| + | |genhide= | ||
| + | |||
| + | |crew=one pilot | ||
| + | |capacity=lots of passengers | ||
| + | |length m=20 | ||
| + | |length ft= | ||
| + | |length in= | ||
| + | |length note=nose probe to tail light | ||
| + | |span m=30 | ||
| + | |span ft= | ||
| + | |span in= | ||
| + | |span note=with extra tips | ||
| + | |upper span m= | ||
| + | |upper span ft= | ||
| + | |upper span in= | ||
| + | |upper span note= | ||
| + | |mid span m= | ||
| + | |mid span ft= | ||
| + | |mid span in= | ||
| + | |mid span note= | ||
| + | |lower span m= | ||
| + | |lower span ft= | ||
| + | |lower span in= | ||
| + | |lower span note= | ||
| + | |swept m=<!-- swing-wings --> | ||
| + | |swept ft=<!-- swing-wings --> | ||
| + | |swept in=<!-- swing-wings --> | ||
| + | |swept note= | ||
| + | |dia m=<!-- airships etc --> | ||
| + | |dia ft=<!-- airships etc --> | ||
| + | |dia in=<!-- airships etc --> | ||
| + | |dia note= | ||
| + | |width m=<!-- if applicable --> | ||
| + | |width ft=<!-- if applicable --> | ||
| + | |width in=<!-- if applicable --> | ||
| + | |width note= | ||
| + | |height m=5 | ||
| + | |height ft= | ||
| + | |height in= | ||
| + | |height note=to top of rudder | ||
| + | |wing area sqm= | ||
| + | |wing area sqft= | ||
| + | |wing area note= | ||
| + | |swept area sqm=<!-- swing-wings --> | ||
| + | |swept area sqft=<!-- swing-wings --> | ||
| + | |swept area note= | ||
| + | |volume m3=<!-- lighter-than-air --> | ||
| + | |volume ft3=<!-- lighter-than-air --> | ||
| + | |volume note= | ||
| + | |aspect ratio=<!-- sailplanes --> | ||
| + | |airfoil=NACA something | ||
| + | |empty weight kg=5000 | ||
| + | |empty weight lb= | ||
| + | |empty weight note=absolutely dry | ||
| + | |gross weight kg=7500 | ||
| + | |gross weight lb= | ||
| + | |gross weight note=all up | ||
| + | |max takeoff weight kg=7800 | ||
| + | |max takeoff weight lb= | ||
| + | |max takeoff weight note=if you must | ||
| + | |fuel capacity=1500 litres | ||
| + | |lift kg=<!-- lighter-than-air --> | ||
| + | |lift lb=<!-- lighter-than-air --> | ||
| + | |lift note= | ||
| + | |more general= | ||
| + | *'''Extra note:''' something else | ||
| + | <!-- | ||
| + | Powerplant | ||
| + | --> | ||
| + | |eng1 number=4 | ||
| + | |eng1 name=Rolls-Whitney AS5 | ||
| + | |eng1 type=turbines | ||
| + | |eng1 kw=<!-- prop engines --> | ||
| + | |eng1 hp=<!-- prop engines --> | ||
| + | |eng1 shp=<!-- prop engines --> | ||
| + | |eng1 kn=5000<!-- jet/rocket engines --> | ||
| + | |eng1 lbf=<!-- jet/rocket engines --> | ||
| + | |eng1 note=at full power | ||
| + | |power original= | ||
| + | |thrust original= | ||
| + | |eng1 kn-ab=<!-- afterburners --> | ||
| + | |eng1 lbf-ab=<!-- afterburners --> | ||
| + | |||
| + | |eng2 number= | ||
| + | |eng2 name= | ||
| + | |eng2 type= | ||
| + | |eng2 kw=<!-- prop engines --> | ||
| + | |eng2 hp=<!-- prop engines --> | ||
| + | |eng2 shp=<!-- prop engines --> | ||
| + | |eng2 kn=<!-- jet/rocket engines --> | ||
| + | |eng2 lbf=<!-- jet/rocket engines --> | ||
| + | |eng2 note= | ||
| + | |eng2 kn-ab=<!-- afterburners --> | ||
| + | |eng2 lbf-ab=<!-- afterburners --> | ||
| + | |||
| + | |eng3 number= | ||
| + | |eng3 name= | ||
| + | |eng3 type= | ||
| + | |eng3 kw=<!-- prop engines --> | ||
| + | |eng3 hp=<!-- prop engines --> | ||
| + | |eng3 shp=<!-- prop engines --> | ||
| + | |eng3 kn=<!-- jet/rocket engines --> | ||
| + | |eng3 lbf=<!-- jet/rocket engines --> | ||
| + | |eng3 note= | ||
| + | |eng3 kn-ab=<!-- afterburners --> | ||
| + | |eng3 lbf-ab=<!-- afterburners --> | ||
| + | |more power= | ||
| + | |||
| + | |prop blade number=<!-- propeller aircraft --> | ||
| + | |prop name= | ||
| + | |prop dia m=<!-- propeller aircraft --> | ||
| + | |prop dia ft=<!-- propeller aircraft --> | ||
| + | |prop dia in=<!-- propeller aircraft --> | ||
| + | |prop dia note= | ||
| + | |||
| + | |rot number=<!-- helicopters --> | ||
| + | |rot dia m=<!-- helicopters --> | ||
| + | |rot dia ft=<!-- helicopters --> | ||
| + | |rot dia in=<!-- helicopters --> | ||
| + | |rot area sqm=<!-- helicopters --> | ||
| + | |rot area sqft=<!-- helicopters --> | ||
| + | |rot area note= | ||
| + | <!-- | ||
| + | Performance | ||
| + | --> | ||
| + | |perfhide= | ||
| + | |||
| + | |max speed kmh=500 | ||
| + | |max speed mph= | ||
| + | |max speed kts= | ||
| + | |max speed note=flat out | ||
| + | |max speed mach=<!-- supersonic aircraft --> | ||
| + | |cruise speed kmh=350 | ||
| + | |cruise speed mph= | ||
| + | |cruise speed kts= | ||
| + | |cruise speed note=nice and gentle | ||
| + | |stall speed kmh=160 | ||
| + | |stall speed mph= | ||
| + | |stall speed kts= | ||
| + | |stall speed note=full flaps and praying | ||
| + | |never exceed speed kmh=800 | ||
| + | |never exceed speed mph= | ||
| + | |never exceed speed kts= | ||
| + | |never exceed speed note=on a good day | ||
| + | |minimum control speed kmh=155 | ||
| + | |minimum control speed mph= | ||
| + | |minimum control speed kts= | ||
| + | |minimum control speed note=whatever this means | ||
| + | |range km=1000 | ||
| + | |range miles= | ||
| + | |range nmi= | ||
| + | |range note=full tank | ||
| + | |combat range km= | ||
| + | |combat range miles= | ||
| + | |combat range nmi= | ||
| + | |combat range note= | ||
| + | |ferry range km= | ||
| + | |ferry range miles= | ||
| + | |ferry range nmi= | ||
| + | |ferry range note= | ||
| + | |endurance=<!-- if range unknown --> | ||
| + | |ceiling m=10000 | ||
| + | |ceiling ft= | ||
| + | |ceiling note= | ||
| + | |g limits=<!-- aerobatic --> | ||
| + | |roll rate=<!-- aerobatic --> | ||
| + | |glide ratio=<!-- sailplanes --> | ||
| + | |climb rate ms=10 | ||
| + | |climb rate ftmin= | ||
| + | |climb rate note=kind of gentle | ||
| + | |time to altitude= | ||
| + | |sink rate ms=<!-- sailplanes --> | ||
| + | |sink rate ftmin=<!-- sailplanes --> | ||
| + | |sink rate note= | ||
| + | |lift to drag= | ||
| + | |wing loading kg/m2= | ||
| + | |wing loading lb/sqft= | ||
| + | |wing loading note= | ||
| + | |disk loading kg/m2= | ||
| + | |disk loading lb/sqft= | ||
| + | |disk loading note= | ||
| + | |fuel consumption kg/km=22 | ||
| + | |fuel consumption lb/mi= | ||
| + | |power/mass= | ||
| + | |thrust/weight= | ||
| + | |||
| + | |more performance= | ||
| + | <!-- | ||
| + | Armament | ||
| + | --> | ||
| + | |armament=<!-- add bulletted list here or if you want to use the following | ||
| + | specific parameters, remove this parameter--> | ||
| + | |guns= | ||
| + | |bombs= | ||
| + | |rockets= | ||
| + | |missiles= | ||
| + | |hardpoints= | ||
| + | |hardpoint capacity= | ||
| + | |hardpoint rockets= | ||
| + | |hardpoint missiles= | ||
| + | |hardpoint bombs= | ||
| + | |hardpoint other= | ||
| + | |||
| + | |avionics= | ||
| + | }} | ||
| + | === (fictional in knots)=== | ||
| + | but only metric in params | ||
| + | |||
| + | {{Aircraft specs | ||
| + | |ref=<!-- reference -->source name | ||
| + | |prime units?=kts<!-- imp or kts first for US aircraft, and UK aircraft pre-metrification, | ||
met(ric) first for all others. You MUST choose a format, or no specifications will show --> | met(ric) first for all others. You MUST choose a format, or no specifications will show --> | ||
<!-- | <!-- | ||
Revision as of 07:56, 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
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
- Service ceiling: 10,000 m (33,000 ft)
- 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: 78 lb/mi (22 kg/km)
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
