Gumnam - Performance

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[ Introduction][ Construction][ Power Plant][ Dimensions][ Performance ][ Uses][ Service and Support]
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:

Stall Speed (with flaps)

45 Km/h

Max Speed level flight

170 Km/h

Min Practical Speed level flight (with flaps)

50 Km/h

Economy Cruise

130 - 140 Km/h

Best Rate of Climb

4.5 meters/sec

Best Glide Ratio

10 to 1

Distance to clear 15 m at Take off

230 meters

Distance to clear 15 m at landing

250 meters

Rolling Distance at Take off

60 meters

Fuel Consumption, average

13 litres/hour

Useful ceiling

12000 ft

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.