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Planes > ToyotaPrevia’s Garage > “Philippine Airlines”

 

ToyotaPrevia’s Profile Photo

ToyotaPrevia

M –26
San Diego, California
United States

 
 

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Challenges 1 – 2 of 2

Challenges W: 1 L: 0

 

Current Challenges

“Philippine Airlines” doesn’t have any current challenges.

Past Challenges

Photo of a 2003 Boeing F-18
The Hornet

2003 Boeing F-18

Owner: Ramair1

  • The Hornet: 5 pts (draw)
  • Philippine Airlines: 5 pts (draw)
  • Total votes: 2
  • Ended: Nov 17, 2011
 
Photo of a 2005 Classified F117 Night Hawk
F117 Night Hawk

2005 Classified F117 Night Hawk

Owner: Ramair1

  • F117 Night Hawk: 4 pts (loss)
  • Philippine Airlines: 6 pts (win)
  • Total votes: 2
  • Ended: Nov 17, 2011
 

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2011 Boeing Hypersonic Jet (Philippine Airlines)

Last updated Nov 6, 2011  

Photo of a 2011 Boeing Hypersonic Jet (Philippine Airlines)

About

Philippine Airlines only Hypersonic Jet Airline

Specs

General characteristics

Crew: 3 (2 Pilots and a flight engineer)
Capacity: 92–120 passengers
(128 in high-density layout)[N 7]
Length: 202 ft 4 in (61.66 m)
Wingspan: 84 ft 0 in (25.6 m)
Height: 40 ft 0 in (12.2 m)
Fuselage internal length: 129 ft 0 in (39.32 m)
Fuselage width: maximum of 9 ft 5 in (2.87 m) external 8 ft 7 in (2.62 m) internal
Fuselage height: maximum of 10 ft 10 in (3.30 m) external 6 ft 5 in (1.96 m) internal)
Wing area: 3,856 ft2 (358.25 m2)
Empty weight: 173,500 lb (78,700 kg)
Useful load: 245,000 lb (111,130 kg)
Powerplant: 4 × Rolls-Royce/SNECMA Olympus 593 Mk 610 afterburning turbojets
Dry thrust: 32,000 lbf (140 kN) each
Thrust with afterburner: 38,050 lbf (169 kN) each
Maximum fuel load: 210,940 lb (95,680 kg)
Maximum taxiing weight: 412,000 lb (187,000 kg)

Concorde G-BOAC

Performance

Maximum speed: Mach 2.04[230] (?1,350 mph, 2,172 km/h) at cruise altitude
Cruise speed: Mach 2.02[230] (?1,320 mph, 2,124 km/h) at cruise altitude
Range: 3,900 nmi (4,500 mi, 7,250 km)
Service ceiling: 60,000 ft (18,300 m)
Rate of climb: 5,000 ft/min (25.41 m/s)
lift-to-drag: Low speed– 3.94, Approach– 4.35, 250 kn, 10,000 ft– 9.27, Mach 0.94– 11.47, Mach 2.04– 7.14
Fuel consumption: 46.85 lb/mi (13.2 kg/km) operating for maximum range
Thrust/weight: 0.373
Maximum nose tip temperature: 260 °F (127 °C)

 

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