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