Difference between revisions of "Template:Aircraft specifications/sandbox/testcases"
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blackwiki>GraemeLeggett (update params) |
blackwiki>GraemeLeggett (→Aircraft with two types of engine (Saunders-Roe SR.177): add diff sort of two types) |
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| − | ==Aircraft with two types of engine ([[Saunders-Roe SR.177]])== | + | ==Aircraft with two types of engine== |
| + | ===Two types no reheat([[Saunders-Roe SR.177]])=== | ||
{{aircraft specifications/sandbox | {{aircraft specifications/sandbox | ||
| Line 282: | Line 283: | ||
|missiles=2 [[de Havilland Firestreak|Firestreak]] air-to-air missiles | |missiles=2 [[de Havilland Firestreak|Firestreak]] air-to-air missiles | ||
|avionics=AI-23 airborne interception [[radar]] | |avionics=AI-23 airborne interception [[radar]] | ||
| + | }} | ||
| + | ===two types and reheat [[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= | ||
| + | |||
}} | }} | ||
Revision as of 12:31, 22 October 2009
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 ()
- Empty weight: 754 kg ()
- 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