[ Introduction][ Construction][ Power Plant][ Dimensions][ Performance ][ Uses][ Service and Support]
PERFORMANCE
At close to sea level, under standard temperature & pressure conditions, with the aircraft loaded to 410 Kg all up weight, and with the 85 BHP Jabiru Engine. The Hanuman performance figures are as follows:
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Stall Speed (with flaps) |
45 Km/h |
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Max Speed level flight |
170 Km/h |
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Min Practical Speed level flight (with flaps) |
50 Km/h |
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Economy Cruise |
130 - 140 Km/h |
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Best Rate of Climb |
4.5 meters/sec |
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Best Glide Ratio |
10 to 1 |
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Distance to clear 15 m at Take off |
230 meters |
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Distance to clear 15 m at landing |
250 meters |
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Rolling Distance at Take off |
60 meters |
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Fuel Consumption, average |
13 litres/hour |
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Useful ceiling |
12000 ft |
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Nil wind range on a standard 80l tank | 800 Km |
Structurally the Hanuman will endure stress up to 6 positive Gs, or 3 negative Gs. This is far beyond the limits to which the Aircraft will be exposed to, even in the most severe turbulent conditions. However, it is important to note that THE HANUMAN IS NOT DESIGNED TO PERFORM AEROBATICS! All components are protected from Corrosion, by Epoxy / Polyurethane Paints, or Electrolytic processes to ensure a safe & long life of structural components even in Coastal Environments.