Difference between revisions of "Template:Aircraft specifications/sandbox/testcases"
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blackwiki>GraemeLeggett (→Specifications (Fairey Rotodyne "Y"): both switch) |
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| − | == | + | {{purge}} |
| + | |||
| + | ==Helicopter ([[Westland Wessex]] HC.2)== | ||
| + | {{aircraft specifications/sandbox| | ||
| + | <!-- if you do not understand how to use this template, please ask at [[Wikipedia talk:WikiProject Aircraft]] --> | ||
| + | <!-- please answer the following questions --> | ||
| + | |plane or copter?=copter | ||
| + | |jet or prop?=prop | ||
| + | <!-- Now, fill out the specs. Please include units where appropriate (main comes first, alt in parentheses). If an item doesn't apply, like capacity, leave it blank. For additional lines, end your alt units with )</li> and start a new, fully-formatted line with <li> --> | ||
| + | |crew=Two pilots (civilian type 60 Wessex cleared for single pilot operation in UK) | ||
| + | |capacity=16 troops or 8 stretchers | ||
| + | |length main=65 ft 8 in | ||
| + | |length alt=20.03 m | ||
| + | |span main=56 ft 0 in | ||
| + | |span alt=17.07 m | ||
| + | |height main=16 ft 2 in | ||
| + | |height alt=4.93 m | ||
| + | |area main=2,463 ft² | ||
| + | |area alt=229 m² | ||
| + | |empty weight main=8,304 lb | ||
| + | |empty weight alt=3,767 kg | ||
| + | |loaded weight main=? lb | ||
| + | |loaded weight alt= ? kg | ||
| + | |max takeoff weight main=13,500 lb | ||
| + | |max takeoff weight alt=6,123 kg | ||
| + | |||
| + | |engine (prop)= [[Rolls-Royce Gnome]] | ||
| + | |type of prop= [[turboshaft]] | ||
| + | |number of props= 2 | ||
| + | |power main= 1,535 shp | ||
| + | |power alt= 1,150 kW | ||
| + | |||
| + | |max speed main=133 mph | ||
| + | |max speed alt=212 km/h | ||
| + | |range main= 480 miles | ||
| + | |range alt= 772 km | ||
| + | |ceiling main=10,000 ft | ||
| + | |ceiling alt=3,050 m | ||
| + | |climb rate main=ft/min | ||
| + | |climb rate alt= m/s | ||
| + | |loading main= 5.5 lb/ft² | ||
| + | |loading alt= 26.7 kg/m² | ||
| + | |power/mass main= 0.11 hp/lb | ||
| + | |power/mass alt= 0.19 kW/kg | ||
| + | }} | ||
| + | |||
| + | ==Gyrodyne - wing and rotor ([[Fairey Rotodyne]])== | ||
{{aircraft specifications/sandbox| | {{aircraft specifications/sandbox| | ||
| Line 51: | Line 97: | ||
}} | }} | ||
| − | == | + | ==aircraft with engines ([[Tarrant Tabor]]) == |
{{aircraft specifications/sandbox | {{aircraft specifications/sandbox | ||
<!-- if you do not understand how to use this template, please ask at [[Wikipedia talk:WikiProject Aircraft]] --> | <!-- if you do not understand how to use this template, please ask at [[Wikipedia talk:WikiProject Aircraft]] --> | ||
| Line 58: | Line 104: | ||
|jet or prop?=prop | |jet or prop?=prop | ||
| − | |ref= | + | |ref= |
|crew=Six | |crew=Six | ||
| Line 116: | Line 162: | ||
}} | }} | ||
| − | == | + | ==aircraft without engines ([[Göppingen Gö 4]])== |
{{aircraft specifications/sandbox | {{aircraft specifications/sandbox | ||
|ref= | |ref= | ||
| Line 129: | Line 175: | ||
|span alt=48 ft 7 in | |span alt=48 ft 7 in | ||
| − | |||
| − | |||
| − | |||
| − | |||
| − | |||
| − | |||
| − | |||
| − | |||
| − | |||
| − | |||
| − | |||
| − | |||
| − | |||
|height main=dunno | |height main=dunno | ||
|height alt= | |height alt= | ||
|wing area main=19 m2 | |wing area main=19 m2 | ||
|wing area alt=204 sq ft | |wing area alt=204 sq ft | ||
| − | + | ||
| − | + | ||
| − | + | |aspect ratio=not given | |
| − | |||
| − | |||
| − | |||
| − | |aspect ratio= | ||
|empty weight main=180 kg | |empty weight main=180 kg | ||
|empty weight alt=400 lb | |empty weight alt=400 lb | ||
|gross weight kg=350 | |gross weight kg=350 | ||
|gross weight lb=770 | |gross weight lb=770 | ||
| − | | | + | |fuel capacity main=not relevant cos its a glider |
| − | | | + | |fuel capacity alt= |
| + | |fuel capacity more=init? | ||
| + | |max speed main= | ||
| + | |max speed alt= | ||
| + | |max speed more=<!-- supersonic aircraft --> | ||
| − | + | |range main= | |
| − | + | |range alt= | |
| − | + | |endurance main=<!-- if range unknown --> | |
| − | + | |endurance alt=<!-- if range unknown --> | |
| − | + | |ceiling main= | |
| − | |range | + | |ceiling alt= |
| − | |range | + | |glide ratio=not given |
| − | |endurance | + | |climb rate main= |
| − | |endurance | + | |climb rate alt= |
| − | |ceiling | ||
| − | |ceiling | ||
| − | |glide ratio= | ||
| − | |climb rate | ||
| − | |climb rate | ||
|sink rate main=<!-- sailplanes -->1.0 m/s | |sink rate main=<!-- sailplanes -->1.0 m/s | ||
|sink rate alt=<!-- sailplanes -->200 ft/min | |sink rate alt=<!-- sailplanes -->200 ft/min | ||
| Line 180: | Line 208: | ||
}} | }} | ||
| − | == | + | ==Aircraft with two types of engine== |
| + | ===Two types no reheat([[Saunders-Roe SR.177]])=== | ||
| + | |||
| + | {{aircraft specifications/sandbox | ||
| + | <!-- if you do not understand how to use this template, please ask at [[Wikipedia talk:WikiProject Aircraft]] --> | ||
| + | <!-- please answer the following questions --> | ||
| + | |plane or copter?=plane | ||
| + | |jet or prop?=both | ||
| + | |||
| + | <!-- Now, fill out the specs. Please include units where appropriate (main comes first, alt in parentheses). If an item doesn't apply, like capacity, leave it blank. For instructions on using |more general=, |more performance=, |power original=, and |thrust original= see [[Template talk:Aircraft specifications]]. To add a new line, end the old one with a right parenthesis ")", and start a new fully formatted line beginning with * --> | ||
| + | |ref= | ||
| + | |crew= one | ||
| + | |capacity= | ||
| + | |length main= 50 ft | ||
| + | |length alt= 15.2 m | ||
| + | |span main= 30 ft | ||
| + | |span alt= 9.1 m | ||
| + | |height main= 14 ft | ||
| + | |height alt= 4.3 m | ||
| + | |area main= | ||
| + | |area alt= | ||
| + | |airfoil= | ||
| + | |empty weight main= | ||
| + | |empty weight alt= | ||
| + | |loaded weight main= 25,500 lb | ||
| + | |loaded weight alt= 11,570 kg | ||
| + | |useful load main= | ||
| + | |useful load alt= | ||
| + | |max takeoff weight main= | ||
| + | |max takeoff weight alt= | ||
| + | |fuel capacity main=not that much | ||
| + | |fuel capacity alt=looks more in litres | ||
| + | |fuel capacity more=but it didn't last long | ||
| + | |more general= | ||
| + | |||
| + | |engine (jet)= [[de Havilland Gyron Junior]] | ||
| + | |type of jet= [[turbojet]] | ||
| + | |number of jets= 1 | ||
| + | |thrust main= 8,000 lbf | ||
| + | |thrust alt= 35.6 kN | ||
| + | |thrust original= | ||
| + | |afterburning thrust main= | ||
| + | |afterburning thrust alt= | ||
| + | |||
| + | |engine (prop)= [[de Havilland Spectre]] | ||
| + | |type of prop= liquid fuel rocket | ||
| + | |number of props= 1 | ||
| + | |power main= 8,000 lbf | ||
| + | |power alt= 35.6 kN | ||
| + | |power original= | ||
| + | |||
| + | |max speed main= 1,550 mph | ||
| + | |max speed alt= 2,500 km/h | ||
| + | |max speed more=estimated | ||
| + | |cruise speed main= | ||
| + | |cruise speed alt= | ||
| + | |never exceed speed main= | ||
| + | |never exceed speed alt= | ||
| + | |stall speed main= | ||
| + | |stall speed alt= | ||
| + | |range main= | ||
| + | |range alt= | ||
| + | |ceiling main=67,000 ft | ||
| + | |ceiling alt= 20,500 m | ||
| + | |ceiling more=estimated | ||
| + | |climb rate main= 60,000 ft/min | ||
| + | |climb rate alt= 18,300 m/s | ||
| + | |climb rate more=estimated | ||
| + | |loading main= | ||
| + | |loading alt= | ||
| + | |thrust/weight= | ||
| + | |power/mass main= | ||
| + | |power/mass alt= | ||
| + | |more performance= | ||
| + | |||
| + | |missiles=2 [[de Havilland Firestreak|Firestreak]] air-to-air missiles | ||
| + | |avionics=AI-23 airborne interception [[radar]] | ||
| + | }} | ||
| + | ===two types and reheat [[Operational Requirement F.155|SR.187]]=== | ||
| + | {{aircraft specifications | ||
| + | |plane or copter?=plane<!-- options: plane/copter --> | ||
| + | |jet or prop?=both<!-- options: jet/prop/both/neither --> | ||
| + | |ref=<ref>[http://www.spaceuk.org/sr53/f155/f155.htm spaceuk.org]</ref> | ||
| + | |crew=2 (pilot and navigator) | ||
| + | |capacity= | ||
| + | |payload main= | ||
| + | |payload alt= | ||
| + | |length main= 83 ft 6 in | ||
| + | |length alt= 25.5 m | ||
| + | |span main=51 ft 7 in | ||
| + | |span alt= 15.7 m | ||
| + | |height main=21 ft 8 in | ||
| + | |height alt= 6.6 m | ||
| + | |area main= | ||
| + | |area alt= | ||
| + | |airfoil= | ||
| + | |empty weight main= 54,700 lb | ||
| + | |empty weight alt= 24,810 kg | ||
| + | |loaded weight main= 97,000 lb | ||
| + | |loaded weight alt= 43,990 kg | ||
| + | |useful load main= | ||
| + | |useful load alt= | ||
| + | |max takeoff weight main= | ||
| + | |max takeoff weight alt= | ||
| + | |more general= | ||
| + | |engine (jet)=de Havilland Gyron P.S.52 | ||
| + | |type of jet=afterburning turbojet | ||
| + | |number of jets=2 | ||
| + | |thrust main=25,000 lb | ||
| + | |thrust alt= 5.6 kN | ||
| + | |thrust original= | ||
| + | |afterburning thrust main=35,000 lb | ||
| + | |afterburning thrust alt= 7.9 kN | ||
| + | |engine (prop)=de Havilland developed Spectre 5 | ||
| + | |type of prop=rocket | ||
| + | |number of props=4 | ||
| + | |power main= 10,000 lb | ||
| + | |power alt= 2.25 kN | ||
| + | |power original= | ||
| + | |max speed main= Mach 2.5 | ||
| + | |max speed alt= | ||
| + | |cruise speed main= | ||
| + | |cruise speed alt= | ||
| + | |stall speed main= | ||
| + | |stall speed alt= | ||
| + | |never exceed speed main= | ||
| + | |never exceed speed alt= | ||
| + | |range main= 260 nm | ||
| + | |range alt= 480 km | ||
| + | |ceiling main=76,000 ft | ||
| + | |ceiling alt= 23,000 m | ||
| + | |climb rate main= | ||
| + | |climb rate alt= | ||
| + | |loading main= | ||
| + | |loading alt= | ||
| + | |thrust/weight= | ||
| + | |power/mass main= | ||
| + | |power/mass alt= | ||
| + | |more performance= | ||
| + | |missiles=OR 3101 (2 radar- and 2 infrared-guided missiles) | ||
| + | |avionics= | ||
| + | |||
| + | }} | ||
| + | |||
| + | ==airship ([[R101]])== | ||
{{aircraft specifications/sandbox | {{aircraft specifications/sandbox | ||
|ref=not given | |ref=not given | ||
| Line 191: | Line 363: | ||
|span main= | |span main= | ||
| − | |span | + | |span alt= |
| − | + | ||
|diameter alt=40 m | |diameter alt=40 m | ||
|diameter main=131 ft | |diameter main=131 ft | ||
| − | |||
| − | |||
| − | |||
|height main= | |height main= | ||
|height alt= | |height alt= | ||
| − | | | + | |area main= |
| − | | | + | |area alt= |
|volume alt= 160,000 m3 | |volume alt= 160,000 m3 | ||
|volume main=5.5 million cubic feet | |volume main=5.5 million cubic feet | ||
| − | |empty weight | + | |empty weight main= |
| − | |empty weight | + | |empty weight alt= |
| − | |gross weight | + | |gross weight main= |
| − | |gross weight | + | |gross weight alt= |
|lift alt=45,000 kg | |lift alt=45,000 kg | ||
|lift main=100,000 lb | |lift main=100,000 lb | ||
| Line 234: | Line 403: | ||
|climb rate main= | |climb rate main= | ||
|climb rate alt= | |climb rate alt= | ||
| + | }} | ||
| + | |||
| + | ==Everything in (made up)== | ||
| + | {{aircraft specifications/sandbox | ||
| + | <!-- if you do not understand how to use this template, please ask at [[Wikipedia talk:WikiProject Aircraft]] --> | ||
| + | |plane or copter?=both<!-- options: plane/copter/both/neither --> | ||
| + | |jet or prop?=both<!-- options: jet/prop/both/neither --> | ||
| + | <!-- Now, fill out the specs. Please include units where appropriate (main comes first, alt in parentheses). If an item doesn't apply, like capacity, leave it blank. | ||
| + | |||
| + | --> | ||
| + | |ref=Someone who wrote a book | ||
| + | <!-- | ||
| + | General characteristics | ||
| + | --> | ||
| + | |crew=5 (Pilot and 4 other guys) | ||
| + | |capacity=lots of stuff | ||
| + | |payload main=13 stone | ||
| + | |payload alt=about 70 kg | ||
| + | |payload more=on a good day | ||
| + | |length main= 100 ft | ||
| + | |length alt= | ||
| + | |span main=100 ft | ||
| + | |span alt= | ||
| + | |||
| + | |diameter main=25 ft | ||
| + | |diameter alt= ? | ||
| + | |height main=20 ft | ||
| + | |height alt=so many metres | ||
| + | |area main= 200 sq yards | ||
| + | |area alt= | ||
| + | |volume main=1,000 cu feet | ||
| + | |volume alt= | ||
| + | |airfoil= Eppler 409 | ||
| + | | root chord = 15 inches | ||
| + | | tip chord = 7 inches | ||
| + | | dihedral = 2.5 degrees | ||
| + | | sweep = 24 degrees | ||
| + | |aspect ratio= | ||
| + | |empty weight main= 754 kg | ||
| + | |empty weight alt= 900 | ||
| + | |loaded weight main= 1,010 kg | ||
| + | |loaded weight alt= about 500 lb | ||
| + | |useful load main= | ||
| + | |useful load alt= | ||
| + | |max takeoff weight main= 1,500 kg | ||
| + | |max takeoff weight alt= | ||
| + | |||
| + | |fuel capacity main=75 imperial gallons | ||
| + | |fuel capacity alt=338 litres | ||
| + | |fuel capacity more=with belly tank | ||
| + | |||
| + | |more general= | ||
| + | <!-- | ||
| + | Powerplant | ||
| + | --> | ||
| + | |engine (jet)=RR Wensum | ||
| + | |type of jet=turbjet | ||
| + | |number of jets=1 | ||
| + | |thrust main= 700 lbf | ||
| + | |thrust alt= | ||
| + | |thrust original= | ||
| + | |afterburning thrust main=1,000 lbf | ||
| + | |afterburning thrust alt= | ||
| + | |||
| + | |engine (prop)=Bristol Eros | ||
| + | |type of prop=piston thingy | ||
| + | |number of props=2 | ||
| + | |power main= 500 hp | ||
| + | |power alt= | ||
| + | |power original= with supercharging | ||
| + | |||
| + | |propeller or rotor?=rotor<!-- options: propeller/rotor --> | ||
| + | |propellers=big flappy ones | ||
| + | |number of propellers per engine= 1 | ||
| + | |propeller diameter main=40 ft 6 inches | ||
| + | |propeller diameter alt= 12.44 metres | ||
| + | <!-- | ||
| + | Performance | ||
| + | --> | ||
| + | |max speed main= 100 mph | ||
| + | |max speed alt= 160 km/h | ||
| + | |max speed more=with a following wind | ||
| + | |cruise speed main= | ||
| + | |cruise speed alt= | ||
| + | |cruise speed more= | ||
| + | |stall speed main= | ||
| + | |stall speed alt= | ||
| + | |stall speed more= | ||
| + | |never exceed speed main= | ||
| + | |never exceed speed alt= | ||
| + | |never exceed speed more= | ||
| + | |minimum control speed main= | ||
| + | |minimum control speed alt= | ||
| + | |minimum control speed more= | ||
| + | |||
| + | lift to drag=low | ||
| + | |||
| + | |range main= 25 miles | ||
| + | |range alt= | ||
| + | |range more=if you don't fill the tank | ||
| + | |combat radius main= | ||
| + | |combat radius alt= | ||
| + | |combat radius more= | ||
| + | |ferry range main= | ||
| + | |ferry range alt= | ||
| + | |ferry range more= | ||
| + | |||
| + | |endurance=call it quits after an hour | ||
| + | |fuel consumption=drinks it | ||
| + | |||
| + | |ceiling main= 1,000 ft | ||
| + | |ceiling alt= 300 m | ||
| + | |ceiling more= | ||
| + | |climb rate main= 100 ft/min | ||
| + | |climb rate alt= | ||
| + | |climb rate more= | ||
| + | |sink rate main= | ||
| + | |sink rate alt= | ||
| + | |sink rate more= | ||
| + | |loading main= | ||
| + | |loading alt= | ||
| + | |thrust/weight= | ||
| + | |power/mass main= | ||
| + | |power/mass alt= | ||
| + | |more performance= | ||
| + | <!-- | ||
| + | Armament | ||
| + | --> | ||
| + | <!-- |armament= if you want to use the following specific parameters, do not use this line at all--> | ||
| + | |guns=4 Brownings | ||
| + | |bombs= 2 x 100 lb MC | ||
| + | |rockets= 4 RP3 | ||
| + | |missiles= none | ||
| + | |hardpoints= 2 | ||
| + | |hardpoint capacity= 100 kg | ||
| + | |hardpoint rockets= | ||
| + | |hardpoint missiles= Black Cat Roman Candles | ||
| + | |hardpoint bombs= | ||
| + | |hardpoint other= | ||
| + | |||
| + | |avionics=*Garmin GPS | ||
| + | |||
}} | }} | ||
==Stuff== | ==Stuff== | ||
{{Reflist}} | {{Reflist}} | ||
Latest revision as of 13:51, 18 October 2020
Script error: No such module "Purge".
Contents
Helicopter (Westland Wessex HC.2)
General characteristics
- Crew: Two pilots (civilian type 60 Wessex cleared for single pilot operation in UK)
- Capacity: 16 troops or 8 stretchers
- Length: 65 ft 8 in (20.03 m)
- Rotor diameter: 56 ft 0 in (17.07 m)
- Height: 16 ft 2 in (4.93 m)
- Disc area: 2,463 ft² (229 m²)
- Empty weight: 8,304 lb (3,767 kg)
- Loaded weight: ? lb (? kg)
- Max. takeoff weight: 13,500 lb (6,123 kg)
- Powerplant: 2 × Rolls-Royce Gnome turboshaft, 1,535 shp (1,150 kW) each
Performance
- Maximum speed: 133 mph (212 km/h)
- Range: 480 miles (772 km)
- Service ceiling: 10,000 ft (3,050 m)
- Rate of climb: ft/min (m/s)
- Disc loading: 5.5 lb/ft² (26.7 kg/m²)
- Power/mass: 0.11 hp/lb (0.19 kW/kg)
Gyrodyne - wing and rotor (Fairey Rotodyne)
General characteristics
- Crew: 2
- Capacity: 48 passengers
- Length: 58 ft 8 in (17.9 m)
- Wingspan: 90 ft 0 in (27.4 m)
- Height: 22 ft 2 in (6.76 m)
- Wing area: 6,360 ft² (591 m²)
- Loaded weight: 33,000 lb (15,000 kg)
- Max. takeoff weight: 38,000 lb (17,000 kg)
- Powerplant:
- 4 × rotor tip jet burning compressed air/fuel, () each
- 2 × Napier Eland turboprops, 2,800 hp (2,100 kW) each
Performance
- Maximum speed: 213 mph (343 km/h)
- Range: 520 mi (830 km)
- Wing loading: 5.2 lb/ft² (25 kg/m²)
- Power/mass (prop): 0.17 hp/lb (280 W/kg)
aircraft with engines (Tarrant Tabor)
General characteristics
- Crew: Six
- Length: 73 ft 2 in (22.31 m)
- Wingspan: 131 ft 3 in (40.02 m)
- Height: 37 ft 3 in (11.36 m)
- Wing area: 4,950 ft² (460 m²)
- Empty weight: 24,750 lb (11,250 kg)
- Loaded weight: 44,672 lb (20,305 kg)
- Powerplant: 6 × Napier Lion 12 cylinder, water cooled broad arrow engines (four tractor, two pusher), 450 hp (336 kW) each
Performance
- Maximum speed: over 96 knots (110 mph, 177 km/h)
- Endurance: 12 hours
- Service ceiling: 13,000 ft (3,970 m)
- Wing loading: 9.02 lb/ft² (44.1 kg/m²)
- Power/mass: 0.06 hp/lb (0.099 kW/kg)
- Climb to 10,000 ft (3,050 m): 33 min 30 sec
Armament
- Bombs: approximately 4,600 lb planned
aircraft without engines (Göppingen Gö 4)
General characteristics
- Crew: Two, pilot and instructor
- Length: 6.74 m (22 ft 1 in)
- Wingspan: 14.8 m (48 ft 7 in)
- Height: dunno ()
- Aspect ratio: not given
- Empty weight: 180 kg (400 lb)
Performance
- sink rate: 1.0 m/s (200 ft/min)
- Glide ratio: not given
Aircraft with two types of engine
Two types no reheat(Saunders-Roe SR.177)
General characteristics
- Crew: one
- Length: 50 ft (15.2 m)
- Wingspan: 30 ft (9.1 m)
- Height: 14 ft (4.3 m)
- Loaded weight: 25,500 lb (11,570 kg)
- Powerplant:
- 1 × de Havilland Gyron Junior turbojet, 8,000 lbf (35.6 kN)
- 1 × de Havilland Spectre liquid fuel rocket, 8,000 lbf (35.6 kN)
Performance
- Maximum speed: 1,550 mph (2,500 km/h) estimated
- Service ceiling: 67,000 ft (20,500 m) estimated
- Rate of climb: 60,000 ft/min (18,300 m/s) estimated
Armament
- Missiles: 2 Firestreak air-to-air missiles
Avionics
AI-23 airborne interception radar
two types and reheat SR.187
Data from [1]
General characteristics
- Crew: 2 (pilot and navigator)
- Length: 83 ft 6 in (25.5 m)
- Wingspan: 51 ft 7 in (15.7 m)
- Height: 21 ft 8 in (6.6 m)
- Empty weight: 54,700 lb (24,810 kg)
- Loaded weight: 97,000 lb (43,990 kg)
- Powerplant:
- 2 × de Havilland Gyron P.S.52 afterburning turbojet, 25,000 lb (5.6 kN) each
- 4 × de Havilland developed Spectre 5 rocket, 10,000 lb (2.25 kN) each
Performance
- Maximum speed: Mach 2.5
- Range: 260 nm (480 km)
- Service ceiling: 76,000 ft (23,000 m)
Armament
- Missiles: OR 3101 (2 radar- and 2 infrared-guided missiles)
airship (R101)
Data from not given
General characteristics
- Crew: 45
- Capacity: 100 passengers
- Length: 777 ft (237 m)
- Wingspan: ()
- Height: ()
- Powerplant: 5 × Beardmore Tornado 8 cylinder Diesel, 585 hp (436 kW) each
Performance
- Maximum speed: 71 mpg (114 km/h)
Everything in (made up)
Data from Someone who wrote a book
General characteristics
- Crew: 5 (Pilot and 4 other guys)
- Capacity: lots of stuff
- Payload: 13 stone (about 70 kg) on a good day
- Length: 100 ft ()
- Wingspan: 100 ft ()
- Height: 20 ft (so many metres)
- Wing area: 200 sq yards ()
- Airfoil: Eppler 409
- Empty weight: 754 kg (900)
- Loaded weight: 1,010 kg (about 500 lb)
- Max. takeoff weight: 1,500 kg ()
- Powerplant:
- 1 × RR Wensum turbjet, 700 lbf ()
- 2 × Bristol Eros piston thingy, 500 hp () with supercharging each
- Propellers: big flappy ones rotor, 1 per engine
- Propeller diameter: 40 ft 6 inches (12.44 metres)
Performance
- Maximum speed: 100 mph (160 km/h) with a following wind
- Range: 25 miles () if you don't fill the tank
- Endurance: call it quits after an hour
- Service ceiling: 1,000 ft (300 m)
- Rate of climb: 100 ft/min ()
- Fuel consumption: drinks it
Armament
- Guns: 4 Brownings
- Hardpoints: 2 with a capacity of 100 kg and provisions to carry combinations of:
- Missiles: Black Cat Roman Candles
- Rockets: 4 RP3
- Missiles: none
- Bombs: 2 x 100 lb MC
Avionics
- Garmin GPS