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OKAVENKO
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The BRM Okavango was projected with the purpose to get a speedy aircraft, extremely robust without loosing the indispensable STOL capacities, to operate on every fields, even those not prepared.
There are two types of engines:
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Rotax 912 UL [80 HP]
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Rotax 912 ULS [100 HP]
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| Characteristics |
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| Wing Span |
8,63 m |
| Wing Surface |
11.20 m2 |
| Lenght |
6,45 m |
| Height |
2,4 m |
| Fuselage width |
1,05 m |
| Reference Weight |
275 Kgs |
| Maximum weight |
284 Kgs |
| Weight with pharachute |
307,5 Kgs |
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Maximum take-off weight |
450 Kgs |
| Wing tank |
76 l |
| Maximum luggage |
25 Kgs |
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| Performances |
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| Version |
Rotax 912 UL |
Rotax 912 ULS |
| Limit of crossed wind |
40 Km/h |
40 Km/h |
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Stall speed |
45 Km/h |
45 Km/h |
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Cruise speed (5000 rpm) |
170 Km/h |
180 Km/h |
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Vz |
1000 fts/min |
1200 fts/min |
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Maximum speed(VNE) |
235 Km/h |
235 Km/h |
| Aproach speed |
70 km/h |
70 km/h |
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Take off distance |
45 m |
40 m |
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Landing distance |
40 m |
40 m |
| Consumption |
12 l |
14 l |
| Autonomy |
6 h |
5h 30 |
| Charge coefficient (at 450 kg) |
+4g / -2g |
+4g / -2g |
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