|
MDM-1 Fox |
 |
Le nouveau FOX arrivé
le 10 mai 2005 à Saint Auban |
General description
|
Manufacturer |
Edward Marganski |
Span |
14,00 m |
45.9 ft |
|
Designer |
E. Marganski, K. Kapinos, H. Gielbaza,
B. Adamski |
Area |
12,34 m2 |
132.8 ft2 |
|
Country of origin |
Poland |
Aspect Ratio |
15,88 |
|
Construction |
Fiberglass |
Empty weight |
345 kg |
761 lb. |
|
First Flight |
1993 |
Gross weight |
525 kg |
761 lb. |
|
Numbers made |
|
Wing Loading |
42,54 kg/m2 |
8.71 LB/ft2 |
|
No. seats |
2 |
L/D |
30 |
126 km/h |
30 |
68 kt |
|
Airfoil |
NACA 64(1)412 |
Min. Sink |
0,80 m/s |
100 km/h |
2.62 ft/s |
54 kt |
The Fox, which first flew in 1993, is a development of the
single-place aerobatic Swift S 1. Although it has been described
as two-place for all jobs, the Fox is optimized for aerobatic
training with erect and inverted clearance of +9/-6 g with one
person and +7/-5 g with two people. The landing gear is fixed,
and approach control is assisted by Schempp-Hirth airbrakes.
Aerobatics information
|
Glider approved according to: ? |
Envelope  |
Speed positive |
G-load Positive |
Speed Inverted |
G-load Inverted |
|
Solo |
Twin |
Solo |
Twin |
|
VA (Max. Maneuver speed) |
215 km/h |
115 kt |
+ 9,0 |
+ 7 |
215 km/h |
115 kt |
- 6 |
- 5 |
|
VNE (Never Exceed speed) |
290 km/h |
155 kt |
? |
(+ 7) |
290 km/h |
155 kt |
? |
(- 5) |
( ) means data is not yet available, but the figure is a quite
probable.
|
Roll Rate according to the manufacturer |
|
|
Seconds for 1 full slow-roll (measured) |
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Flick/Snap/Quick maneuvers |
Inverted spin |
Inverted half loop |
Inverted loop |
Inverted Cuban Eight |
Tail slide |
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Solo |
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Two occupants |
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Maneuvers described in the manual:
Maneuvers described as not permitted in the manual:
