Performance Specs

Performance Charts

Flight Time v. Payload

Thrust-to-weight ratio

Flight Time (min)	Payload (lbs)	Payload (kg)	Total Weight (lbs)	Thrust to Weight Ratio
50	0	0	43.28	3.5
41.7	5	2.3	48.28	3.1
33.3	10	4.5	53.28	2.8
26.6	15	6.8	58.28	2.6
22	20	9.1	63.28	2.4
18	25	11.3	68.28	2.2
12.5	30	13.6	73.28	2.0
10.75	35	15.9	78.28	1.9

Maximum Gross Weight

To determine maximum gross weight, determine flight location pressure altitude, and temperature, and refer to the weight in the chart below. Gross Weight includes payload, battery, and structure weight.

The maximum gross weight might exceed the weight allowed by regulatory agencies. When determining gross weight, please consider any such local restrictions on aircraft weight when planning aircraft weight.

The maximum gross weight at a defined density altitude was established by calculating weight so that sufficient thrust margin for maneuvering is maintained.

Cells highlighted in yellow indicate where the weight is limited by the maximum design weight

Max Configurable Parameters
Max Angular Velocity	Configurable, default to 100 deg/s in manual mode
Max Pitch Angle	Configurable, default to
Max Ascent Speed (by mode)	Configurable, default to 6m/s in Position & Altitude Mode
Max Descent Speed (vertical (by mode)	Configurable, default to 4m/s down in Position & Alt Mode
Max Speed (by mode)	Configurable, default to 20m/s in Position Mode
Max Service Ceiling above Sea Level	Depends on payload, see "Maximum Gross Weight" chart