The Avro Canada TS-140 was a proposed by Avro Canada to the United States Navy TS-140 Specification in 1956. The TS-140 was a canard type aircraft to be powered by four Bristol Orpheus jet engines. However the USN selected the Bell D-188A proposal instead.

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General characteristics
Crew: 1, pilot
Length: 15.24 m (50 ft)
Wingspan: 7.70 m, Canards 5.56 m (25.25 ft, Canards 18.25 ft)
Height: 2.97 m (9.75 ft)
Wing area: 66 m² Including Canards (215 ft² Including Canards)
Empty weight: 4663 kg (10,280 lb)
Loaded weight: 6464 kg (14,250 lb)
Max. takeoff weight: 7371 kg (16,250 lb)
Powerplant: 4 × Bristol Orpheus 801 turbojets, 22 kN (4,850 lbf) each

Performance
Maximum speed: 2115 km/h (1314 mph est.)
Service ceiling: 18,288 m (60,000 ft est.)
Rate of climb: 926.7 m/s at Mach 0.9 (55,600 ft/min at Mach 0.9 est.)
Thrust/weight: 1.1 est.

Armament


4x AIM-9 Sidewinder