UAV Analysis V1.0

by Barnard Microsystems Limited

Range = R

Km

INPUT

 

   

 

Take-off weight = Wto

Kg

INPUT

 

   

 

Wfuel

Kg

INPUT

 

   

 

endurance speed

Kph

INPUT

 

   

 

 

typically between 80 … 120 Kph

 

   

 

Wingspan

m

calculated

 

   

 

length

m

calculated

 

   

 

Wairframe

Kg

calculated

 

   

 

Wfuel calculated from R and Wto

Kg

calculated

 

   

 

Characteristic distance "D"

Km

calculated

 

   

 

endurance

hours

calculated

 

   

 

maximum engine power

Kwatts

calculated

 

   

 

4 stroke engine capacity

cc

calculated

 

   

 

4 stroke engine weight

Kg

calculated

 

   

 

payload weight

Kg

calculated