Period
|
1960's
|
Designation
|
C.102B Jetliner II
|
First Flight
|
25 May 1965
|
Manufacturer
|
A.V. Roe Canada, Ltd.
|
# Constructd (including prototype)
|
135
|
Wing Span
|
29.9 m (98 ft 1 in)
|
Overall Length
|
28 m (91.86 ft)
|
Overall Height
|
8.1 m (26 ft 51/2 in)
|
Weight (dry)
|
19 425 kg (42 824.79 lbs)
|
Weight (gross)
|
33 722 kg (74 344.28 lbs)
|
Cruising Speed
|
720 km/h (447.39 mp/h)
|
Maximum Speed
|
850 km/h (528.17mp/h)
|
Rate Of Climb
|
700 m (2 296.59 ft)/minute
|
Service Ceiling
|
13 716 m (45 000 ft)
|
Range
|
4 828.03 km (3 000 mi)
|
Power Plants
|
4 x Orenda 11 (3 299.88 kg (7 275 lbs)), each, static thrust centrifugal turbojet engines
|
Immediate Competition
|
Boeing 707
|
Period
|
1970's
|
Designation
|
C.102C Jetliner III
|
First Flight
|
19 December 1972
|
Manufacturer
|
A.V. Roe Canada, Ltd.
|
# Constructd (including prototype)
|
349
|
Wing Span
|
29.9 m (98 ft 1 in)
|
Overall Length
|
28 m (91.86 ft)
|
Overall Height
|
8.1 m (26 ft 51/2 in)
|
Weight (dry)
|
29 722 kg (65 525.79 lbs)
|
Weight (gross)
|
42 000 kg (92 594.15 lbs)
|
Cruising Speed
|
1 046.07 km/h (650 mp/h)
|
Maximum Speed
|
1 367.94 km/h (850 mp/h)
|
Rate Of Climb
|
13 563.60 m (44 500 ft)/minute from Sea Level
|
Service Ceiling
|
16 764 m (55 000 ft)
|
Range
|
7 563.92 km (4 700 mi)
|
Power Plants
|
2 x Orenda PS-13 Iroquois (8 731.65 kg (19 250 lbs) base thrust -- 11 793.40 kg (26 000 lbs) with afterburner) each, static thrust centrifugal turbojet engines
|
Immediate Competition
|
Boeing 707
|
