Period
|
Postwar
|
Designation
|
XC.102
|
First Flight
|
10 August 1949
|
Manufacturer
|
A.V. Roe Canada, Ltd.
|
# Constructd (including prototype)
|
1
|
Wing Span
|
29.9 m (98 ft 1 in)
|
Overall Length
|
25.1 m (82 ft 5 in)
|
Overall Height
|
8.1 m (26 ft 51/2 in)
|
Weight (dry)
|
16 783 kg (37 000 lbs)
|
Weight (gross)
|
29 484 kg (65 000 lbs)
|
Cruising Speed
|
676 km/h (500 mp/h)
|
Maximum Speed
|
805 km/h (500 mp/h)
|
Rate Of Climb
|
677 m (2 200 ft)/minute
|
Service Ceiling
|
12 283 m (40 000 ft)
|
Range
|
2 000 km (1 250 mi)
|
Power Plants
|
4 x Rolls-Royce Derwent 5/17 (1 633 kg (3 600 lbs)) static thrust centrifugal turbojet engines
|
Immediate Competition
|
DeHavilland Comet
|
