reply to post by The Winged Wombat
The Osprey programe has always had problems with downwash and alot of concern with its for and unpredicablity. In 1995 in testing there was concern
over OT-IIA and the amount of downwash and its effect in roped extraction or deployment. From the sounds of it the downwash issue though has been more
or less sorted since 2000 or so with the concluding of test in 2001-2 as well. Not sure how exactly the issue was addressed but as you said they seem
to still be finding little things to do with it from time to time
Also to expand on the speed differences of the STOL aircraft to the Osprey to the Chinook.
Caribou Performance
Maximum speed: 216 mph (348 km/h)
Range: 1,307 mi (2,103 km)
Service ceiling: 24,800 ft (7,559 m)
Rate of climb: 1,355 ft/min (413 m/min)
Buffalo Performance
Maximum speed: 290 mph (467 km/h)
Range: 690 miles (1,110 km)
Service ceiling: 31,000 ft (9,450 m)
-------------------------
Osprey Performance
Maximum speed: 275 knots (316 mph, 509 km/h)
Range: 879 nmi (1,011 mi, 1,627 km) (unrefueled)
Service ceiling: 26,000 ft (7,925 m)
Rate of climb: 2,320 ft/min (11.8 m/s)
------------------------
Chinook Performance
Maximum speed: 170 kn VNE (196 mph, 315 km/h)
Range: 1,259 mi (1,110 NM, 2,060 km)
Service ceiling: 18,500 ft (5,640 m)
Rate of climb: 1,980 ft/min (10.1 m/s)
Interesting to note that the Osprey is 26 mph faster then a normal pourpose built aircraft like the Buffalo. Hmmmm Maybe Canada should look into a
couple for SAR as well as complement any Chinooks we get (wishful thinking

)
[edit on 22/08/06 by Canada_EH]