sUAS Performance Analyzer Application (sUPA App.) V1.0
Created by Andrew Jesus, 2025
Requirement Set
Which Year of AERE 4600's Requirements?
StarCCM Data
Planform Area (ft
2
):
Coefficient Lift Curve Slope:
x +
Coefficient Drag Curve Equation:
x
4
+
x
3
+
x
2
+
x +
Other Aircraft Information
Aircraft Dry Weight (lb):
Payload Weight (0-1.5lbs):
Propulsion Setup
Upload Propulsion Data?
Number of Motor(s)
Please input Motocalc folder with desired throttle data(s):
Note: The files in the folder need to be named just the throttle %
ex ("30.txt" "50.txt" "100.txt")
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