Maximum limiting Mach number
Maximum level speed
Ceiling
Range
Fuselage length
Height
Wing Span
Wing Area
Tailplane, nett area
Fin & rudder nett area
Rudder area
Undercarriage track
Engine type
maximum thrust
Fuel Capacity, internal
Fuel Capacity, external
Weight empty
Maximum Take-Off Weight Aircraft Clean: SL to 20,000 feet
Aircraft Clean: SL to 40,000 feet
Aircraft with slipper tanks: SL to 20,000 feet
Aircraft with slipper tanks: SL to 40,000 feet |
|
1.3 Mach
0.95 Mach (525 knots IAS at SL, 636 mph)
48,000 ft.
1,151 miles (with two 300-liter under wing tanks)
31ft. 9in. (without probe)
9ft. 7.5in.
24ft. 0in.
175 sq. feet
37.10 sq. feet
20.25 sq. feet
3.75 sq. feet
5ft. 1in.
Orpheus 101
4,520 lbs. at 9,660 rpm at SL.
268 IG
118 IG
5,560 lbs.
9,520 lbs.
3.5 minutes
7.5 minutes
4 minutes
9 minutes |
