International Journal of Aerospace Engineering / 2021 / Article / Tab 3

Research Article

A Computational Design Analysis of UAV’s Rotor Blade in Low-Temperature Conditions for the Defence Applications

Table 3

Operational mission profile.

Altitudes (m)TemperatureRPM droneVelocity (m/s)

Zone-10050008
Zone-2250-25°C55008
Zone-3500-50°C60008
Zone-4750-75°C65008
Zone-51000-100°C70008

The altitude and temperatures are taken from above 6000 m from the sea level.