UAS OSC Volume 2

WARNING: This document was generated automatically and may contain errors and/or ommissions. You MUST review the data and satisfy yourself that it is complete and accurate. There is a link to the original source of the data below to help you do that.

Operator ID:
UAS Operating Safety Case Volume 2 - UAS Description:
Document reference number:
Document version and date:

Amendment record

Amendment Number	Date	Amended by	Details of changes

CAP722A Table 6

Aircraft and systems description

UAS Model	Inspire 3
UAS design & manufaturing organisations	DJI

UAS physical characteristics

Empty Mass
Maximum Take-Off Mass (MTOM)	Max Takeoff Weight: Approx. 4,310 g
Dimensions for Rotorcraft / Multirotor
Length of aircraft body	Diagonal Distance: Landing Gear Raised: 695 mm Landing Gear Lowered: 685 mm
Width of aircraft body
Height of aircraft body
Propeller Configuration	Propeller Model: Standard Propellers: DJI 1671 High-Altitude Propellers: DJI 1676
Propeller Dimensions
Sound power level
Any other relevant information

CAP722A Table 7

UAS performance characteristics

Maximum airspeed	Max Horizontal Speed (at sea level, no wind): 94 kph Measured when flying in a windless environment at sea level, with gimbal camera and lens attached to the aircraft and without other accessories. This data is for reference only.
Minimum airspeed to maintain safe flight
Normal/typical operating height
Maximum operating height	Max Service Ceiling Above Sea Level: Standard Propellers: 3800 m High-Altitude Propellers: 7000 m Measured in an environment with light wind with the gimbal camera and lens attached to the aircraft and without other accessories. This data is for reference only.
Maximum flight time during normal operation	Max Flight Time: Approx. 28 minutes (landing gear lowered) Approx. 26 minutes (landing gear raised) Measured when flying forward at a constant speed of 36 kph in a windless environment at sea level, with gimbal camera and lens attached to the aircraft and without other accessories, and recording 4K/24fps H.264 (S35) video until the battery reached 0%. This data is for reference only. Please refer to the actual values in the app.
Maximum flight time on an ISA day at cruising speed at normal/typical operating height.
Maximum flight range on an ISA day (normal and emergency conditions)
Glide distances
Maximum radio range of the C2 Link

CAP722A Table 8

UAS environmental limitations

Wind speed limits	Max Wind Resistance: Takeoff/land: 12 m/s In-flight: 14 m/s Measured when flying at sea level, with gimbal camera and lens attached to the aircraft and without other accessories. This data is for reference only.
Turbulence restrictions
Precipitation limits
OAT limits	Operating Temperature: -20 Deg. to 40 Deg. C (-4 Deg. to 104 Deg. F)
In-flight icing condition limits
Any other relevant information

CAP722A Table 9

Construction

Type of material
Material characteristics or properties
Any other relevant information

CAP722A Table 10

Electrical power system

Batteries:
Battery type, model and manufacturer	Capacity: 4280 mAh Type: Li-ion Chemical System: LiCoO2 Model: TB51 Intelligent Battery
Quantity
Arrangement
Generator:
Generator type, model and manufacturer
Specification
Electrical loads	Nominal Voltage: 23.1 V Energy: 98.8 Wh
Electrical load shedding functionality
Power supply redundancy
Procedures to charge and discharge batteries.
Safety provisions with regards to hazards inherent to high-voltage storage devices:
Procedures in place for safe handling by any person who may come into contact with high-voltage storage devices
Means of identifying high-voltage storage
Safety provisions for any person discovering the UA following an accident.
Procedures and safety provisions to mitigate the risk of battery thermal runaway.
Procedures for monitoring high-voltage storage devices.
HMI:
Information indicated to the remote pilot.
Alert messages indicated to the remote pilot.
Any other relevant information	Charging Temperature: -20 Deg. to 40 Deg. C (-4 Deg. to 104 Deg. F) If the temperature of the battery is lower than 10 Deg. C (50 Deg. F), the battery will trigger an auto-heating function. Charging in a low-temperature environment below 0 Deg. C (32 Deg. F) may shorten battery life. Operating Temperature: -20 Deg. to 40 Deg. C (-4 Deg. to 104 Deg. F)

CAP722A Table 11

Propulsion system

Propulsion type	Motor Model: DJI 3511s
Engines:
Type, model and manufacturer
Propeller type, model and manufacturer
Quantity
Arrangement
Power output
Propeller guards
In-flight restart functionality
Performance monitoring
Health monitoring
Safety features and redundancy in the system that allow maintaining flight after a failure or degradation has occurred in the propulsion system.
Fuel-powered propulsion system – Safety features to mitigate the risk of engine loss when the following hazards occur:
Fuel starvation
Fuel contamination
Failed signal input from the control station
Engine controller failure
Indication to the remote pilot
Electric-powered propulsion system:
Power source and supply management with regards to other systems in the UA
Redundant power sources
Maximum continuous power output of the motor
Maximum peak power output of the motor
Electrical distribution architecture
Electrical load shedding functionality
HMI:
Information indicated to the remote pilot.
Alert messages indicated to the remote pilot.
Any other relevant information

CAP722A Table 12

Fuel system

Fuel type
Safety provisions with regards to hazardous substances within the fuel system:
List of hazardous substances and their characteristics.
Procedures in place for safe handling of the UA by any person who may come into contact with the hazardous substances.
Means of identifying the hazardous substances.
Safety provisions for any person discovering the UA following an accident.
HMI:
Information indicated to the remote pilot.
Alert messages indicated to the remote pilot.
Any other relevant information

CAP722A Table 13

Flight Controls system

Design and operation of flight control units, surfaces, actuators, control linkages, etc.
Flight controller:
Type, model and manufacturer	Model: RM700B
Functions
Flight modes available
Automatic functions:
Take-off and landing
Stabilisation
Autopilot
Return to home
If functions are provided by COTS equipment, provide type, model and manufacturer.
Safety features and redundancy in the system which allow maintaining flight after a failure or degradation of the flight control system, including indication to the remote pilot.
HMI:
Information indicated to the remote pilot.
Alert messages indicated to the remote pilot.
Any other relevant information

CAP722A Table 14

Navigation

Sensors
Type, model and manufacturer	Global Navigation Satellite System: GPS + Galileo + BeiDou
Quantity
Telemetry links
Method to determine current position.	RTK Positioning Accuracy (fixed RTK enabled): 1 cm + 1 PPM (horizontal) 1.5 cm + 1 PPM (vertical)
Method to navigate to intended destination.
Automatic/automated navigation functions
Geo-awareness functions
Containment functions
Safety features and redundancy in the system which allow maintaining flight after a failure or degradation has occurred in the navigation system:
Backup means of navigation
Detection of and response to loss of primary means and secondary means of navigation.
Indication to the remote pilot
HMI:
Information indicated to the remote pilot.
Alert messages indicated to the remote pilot.
Any other relevant information

CAP722A Table 15

Detect and Avoid (DAA) systems

DAA system functions	Forward: Measurement Range: 1.5-48 m Effective Sensing Speed: <=15 m/s FOV: Horizontal 90 Deg., Vertical 103 Deg. (landing gear raised) Horizontal 72 Deg., Vertical 103 Deg. (landing gear lowered) Backward: Measurement Range: 1.5-48 m Effective Sensing Speed: <=15 m/s FOV: Horizontal 90 Deg., Vertical 103 Deg. Lateral: Measurement Range: 1.5-42 m Effective Sensing Speed: <=15 m/s FOV: Horizontal 90 Deg., Vertical 85 Deg. Upward: Measurement Range: 0.2-13 m Effective Sensing Speed: <=6 m/s FOV: Front and Back 100 Deg., Left and Right 90 Deg. Downward: Measurement Range: 0.3-18 m Effective Sensing Speed: <=6 m/s FOV: Front and Back 130 Deg., Left and Right 160 Deg.
Devices used
Technology used
Interface between the DAA system and the flight control computer
Limitations of the DAA system	Operating Environment: Forward, Backward, Left, Right, and Upward: surfaces with discernible patterns and adequate lighting (lux >15) Downward: surfaces with discernible patterns and diffuse reflectivity >20% (e.g., walls, trees, people); adequate lighting (lux >15) Obstacle sensing is disabled while the landing gear is in the process of being raised or lowered.
Evidence of equipment qualification and approval.
DAA event sequence:
Level of automation
Actions required by the remote pilot
Means to verify normal system operation.
HMI:
Information indicated to the remote pilot.
Alert messages indicated to the remote pilot.
Any other relevant information

CAP722A Table 16

Other avionics systems

Command Unit (CU)

Power sources, supply management and redundancy.	Battery: Built-in Battery: 3250mAh-7.2V (a set) External Battery: WB37 Intelligent Battery
Radio signal:
Determination of the signal strength and health value.
Threshold values which represent a critically degraded signal.
Control handover between two CUs
Safety features to mitigate the risk of inadvertent command activation:
List of critical commands
Mitigation means
Safety features to mitigate the risk of display or HMI lock-up.
Safety features to maintain flight-critical processing when multiple programs are running concurrently.
HMI:
Information indicated to the remote pilot.
Radio signal strength and/or health indication to the remote pilot.
Alert messages indicated to the remote pilot.
Any other relevant information	Operating Temperature: -20 Deg. to 50 Deg.C (-4 Deg. to 122 Deg. F)

CAP722A Table 17

Command an Control (C2) link

RLOS
BRLOS
Antennas:
Type, model and manufacturer
Locations on the UAS
Transceivers / Modems:
Power levels
Transmission schemes
Operating frequencies
Details of frequency spectrum approvals	Operating Frequency: 2.4000-2.4835 GHz 5.725 GHz-5.850 GHz In some countries and regions, 5.1GHz and 5.8GHz frequencies are prohibited, or the 5.1GHz frequency is only allowed for indoor use. Please refer to local laws and regulations.
Maximum power output/range
Type of signal processing
Datalink margin in terms of the overall link bandwidth at the maximum anticipated distance from the CU.
Operational C2 link management:
Frequency switchovers
Contingency situations
Third party link service provider
Radio signal:
Determination of the signal strength and health value
Threshold values which represent a critically degraded signal.
Minimum and average assured data rates
Minimum and average assured latencies
Design features and procedures to maintain availability, continuity, and integrity of the datalink:
RF or other interference
Flight beyond communications range
Antenna masking
Loss of CU functionality
Loss of UA functionality
Atmospheric attenuation
Safety features to mitigate the risk of loss of C2 link:
C2 links redundancy
Automatic triggering of an emergency recovery function
Automatic return to home
Safety features to mitigate the risk of harmful interference.
HMI:
Information indicated to the remote pilot.
Radio signal strength and/or health indication to the remote pilot.
Alert messages indicated to the remote pilot.
Any other relevant information

CAP722A Table 18

Communications

Antennas:
Type, model and manufacturer
Locations on the UAS
Communication method:
VHF
GSM network
Satellite
Safety features to mitigate the loss of communication function:
Primary communication means
Secondary / back-up communication means
HMI:
Information indicated to the remote pilot.
Radio signal strength and/or health indication to the remote pilot.
Alert messages indicated to the remote pilot.
Any other relevant information

CAP722A Table 19

Take-off and landing mechanisms

Wheels, skids, rails, launchers, etc.
If various mechanisms can be fitted:
Primary mechanism
Secondary mechanisms
Operational conditions/requirements for each mechanism.
Any other relevant information

CAP722A Table 20

Emergency recovery and safety systems

Mode of operation
Safety features which mitigate the risk of loss of control or situational awareness.
Means to verify normal system operation.
HMI:
Information indicated to the remote pilot.
Alert messages indicated to the remote pilot.
Any other relevant information

CAP722A Table 21

External lighting

Type, model and manufacturer
Locations on the UA
Colour
Operation
Operating modes
Purpose
HMI:
Information indicated to the remote pilot.
Alert messages indicated to the remote pilot.
Any other relevant information

CAP722A Table 22

Payload

Types
Mass
Interfaces with the UA:
Mechanical interface
Electrical interface
Data interface
Release mechanism
Any other interface
Procedures to install the payload onto the UA.
Effects of the payload on the UA
Sensors
Safety features to mitigate the risk of the payload affecting the flight of the UA:
Effects on aerodynamics
Effects of electro-magnetic interference.
Effects of electrical power and / or data connection failures on the UAS.
Effects of complete detachment of the payload from the UA (either caused by a failure or through intentional lowering / dropping of the payload).
Effects of partial detachment of the payload from the UA.
Distraction of the remote pilot generated by the payload during flight.
Procedures to verify the attachment points to the UA.
Procedures to verify the UA MTOM and CG location.
Procedures to detect and mitigate any failure of the payload in flight.
Safety provisions with regards to hazards inherent to the payload
Procedures in place for safe handling of the payload.
Means of identifying hazards.
HMI:
Information indicated to the remote pilot.
Alert messages indicated to the remote pilot.
Any other relevant information

CAP722A Table 23

Ground support equipment

UAS launch and recovery systems
Power sources
Transportation equipment
Backup or emergency equipment
Procedures to transport UA, CU, battery/fuel, and other equipment between operation sites and from the loading/off-loading area to the take-off/landing area.
Storage of ground support equipment.
Suitability of the ground support equipment and transportation method with regards to the UAS components’ fragility, sensitivity or inherent hazards.
Ground support equipment standards
Ground support equipment manufacturer's recommendations.
Any other relevant information

CAP722A Table 24

Maintenance

Maintenance manual:
Structure
Maintenance procedures:
Inspections
Overhaul
Repairs
Assurance of repair procedures
Batteries maintenance during storage periods
Origin of each procedure
Maintenance schedules
Procedures to record maintenance that has been carried out.
Storage of maintenance records
Staff qualification and levels of approval.
Procedures to use the manual by the Maintenance staff
Configuration control
Any other relevant information

CAP722A Table 25

Spare parts procurement

Sources of procurement
Process to confirm the suitability of the part.
Any other relevant information

CAP722A Table 26

Change Management and modifications to the system

Hardware, software, and firmware version control
Modification standards
Modification records storage
Safety assessment associated with the modification
Any other relevant information

CAP722A Table 27

Safety features of the UAS

Step 1 – Identify the main functions of the UAS.
Step 2 – Identify the sub-functions.
Step 3 – Consider the ways each function may fail.
Step 4 – Identify the failure conditions.
Step 5 – Select those failure conditions that may lead to mid-air collision or harm to uninvolved people on the ground. (Identified Hazard)
Step 6 – Assurance
Step 7 – Describe the consequence of the failure condition.
Step 8 – Describe the failure modes. (Unmitigated Failures)
Step 9 – Identify the single points of failure.
Step 10 – Describe the risk mitigation means.

CAP722A Table 28

ANNEX - Manufacturer supplied data forDJI Inspire 3

Aircraft
Model	T740
Startup Time	Approx. 3,995 g (includes gimbal camera, two batteries, lens, PROSSD, and propellers)
Max Takeoff Weight	Approx. 4,310 g
Hovering Accuracy Range	Vertical: ±0.1 m (with vision positioning) ±0.5 m (with GNSS positioning) ±0.1 m (with RTK positioning) Horizontal: ±0.3 m (with vision positioning) ±0.5 m (with GNSS positioning) ±0.1 m (with RTK positioning)
RTK Positioning Accuracy (fixed RTK enabled)	1 cm + 1 PPM (horizontal) 1.5 cm + 1 PPM (vertical)
Max Angular Velocity	Pitch: 200 Deg./s Roll: 200 Deg./s Yaw: 150 Deg./s
Max Tilt Angle	N Mode: 35 Deg. S Mode: 40 Deg. A Mode: 35 Deg. T Mode: 20 Deg. Emergency Brake: 55 Deg.
Max Ascent Speed	8 m/s Measured when flying in a windless environment at sea level, with gimbal camera and lens attached to the aircraft and without other accessories. This data is for reference only.
Max Descent Speed	Vertical: 8 m/s Tilt: 10 m/s Measured when flying in a windless environment at sea level, with gimbal camera and lens attached to the aircraft and without other accessories. This data is for reference only.
Max Horizontal Speed (at sea level, no wind)	94 kph Measured when flying in a windless environment at sea level, with gimbal camera and lens attached to the aircraft and without other accessories. This data is for reference only.
Max Service Ceiling Above Sea Level	Standard Propellers: 3800 m High-Altitude Propellers: 7000 m Measured in an environment with light wind with the gimbal camera and lens attached to the aircraft and without other accessories. This data is for reference only.
Max Wind Resistance	Takeoff/land: 12 m/s In-flight: 14 m/s Measured when flying at sea level, with gimbal camera and lens attached to the aircraft and without other accessories. This data is for reference only.
Max Hovering Time	Approx. 25 minutes Measured when hovering in a windless environment at sea level with gimbal camera and lens attached to the aircraft and without other accessories, with landing gear raised, and recording 4K/24fps H.264 (S35) video until the battery reached 0%. This data is for reference only. Please refer to the actual values in the app.
Max Flight Time	Approx. 28 minutes (landing gear lowered) Approx. 26 minutes (landing gear raised) Measured when flying forward at a constant speed of 36 kph in a windless environment at sea level, with gimbal camera and lens attached to the aircraft and without other accessories, and recording 4K/24fps H.264 (S35) video until the battery reached 0%. This data is for reference only. Please refer to the actual values in the app.
Motor Model	DJI 3511s
Global Navigation Satellite System	GPS + Galileo + BeiDou
Propeller Model	Standard Propellers: DJI 1671 High-Altitude Propellers: DJI 1676
Operating Temperature	-20 Deg. to 40 Deg. C (-4 Deg. to 104 Deg. F)
Diagonal Distance	Landing Gear Raised: 695 mm Landing Gear Lowered: 685 mm
Travel Mode Dimensions	Height: 176 mm Width: 709.8 mm Length: 500.5 mm
Controller
Max Non-Vertical Descent Speed	35mm full-frame CMOS
Max Horizontal Speed with Obstacle Avoidance	Photo: 8192 x 5456 Video: 8192 x 4320
Max Gust Handling	View detailed list
Processors	DL 18 mm F2.8 ASPH Lens DL 24 mm F2.8 LS ASPH Lens DL 35 mm F2.8 LS ASPH Lens DL 50 mm F2.8 LS ASPH Lens
Operational Temperature Range	JPG, DNG
Wireless Range (no interference, line of sight operation)	MOV, CinemaDNG
Wireless Networking (media offload)	Capture, Record, Playback
Obstacle Avoidance Coverage	P, A, S, M
Controller Dimensions	Electronic shutter
Screen	8-1/8000 s
Dimensions	AWB MWB (2000K-10000K)
Weight	Photo ISO: 100-25600 Video EI: 200-6400
Max Range	Capture Mode: Auto, 50 Hz, 60 Hz, OFF
Operating Frequencies	Hovering: ±0.002 Deg. Flying: ±0.004 Deg.
Transmitter Power (EIRP)	Quick release
Ingress Protection Rating	Tilt: -128 Deg. to +110 Deg. (landing gear lowered) -148 Deg. to +90 Deg. (landing gear raised) Roll: -90 Deg. to +230 Deg. Pan: ±330 Deg.
Operating Time	Tilt (landing gear lowered): Before gimbal tilt limit extension: -90 Deg. to +30 Deg. After gimbal tilt limit extension: -115 Deg. to +100 Deg. Tilt (landing gear raised): Before gimbal tilt limit extension: -90 Deg. to +30 Deg. After gimbal tilt limit extension: -140 Deg. to +75 Deg. Roll: ±20 Deg. Pan: ±300 Deg.
Battery	With DJI RC Plus: Tilt: 120 Deg./s Roll: 180 Deg./s Pan: 270 Deg./s With DJI Master Wheels: Tilt: 432 Deg./s Roll: 432 Deg./s Pan: 432 Deg./s
GNSS	Approx. 516 g (without lens)
Video Transmission
Video Transmission System	O3 Pro
Live View Quality	FPV Camera: Up to 1080p/60fps Gimbal Camera: Up to 1080p/60fps, 4K/30fps
Operational Temperature Range	50 Mbps
Max Transmission Distance (free of interference)	Single Control Mode: FPV Camera: approx. 15 km (FCC), 8 km (CE/SRRC/MIC) Gimbal Camera (1080p/60fps live feeds): approx. 13 km (FCC), 7 km (CE/SRRC/MIC) Gimbal Camera (4K/30fps live feeds): approx. 5 km (FCC), 3 km (CE/SRRC/MIC) Dual-Control Mode: FPV Camera: approx. 12 km (FCC), 6.4 km (CE/SRRC/MIC) Gimbal Camera (1080p/60fps live feeds): approx. 11.2 km (FCC), 5.6 km (CE/SRRC/MIC) Gimbal Camera (4K/30fps live feeds): approx. 4 km (FCC), 2.4 km (CE/SRRC/MIC) Measured in an unobstructed outdoor environment free of interference, with gimbal camera and lens attached to the aircraft and without other accessories. The above data shows the farthest communication range for one-way, non-return flights under each standard. During your flight, please pay attention to reminders in the app.
Lowest Latency	FPV Camera: 90 ms Gimbal Camera: 90 ms The lowest latency of the gimbal camera was measured when recording 4K/60fps ProRes RAW video. The lowest latency of the FPV camera was measured with strong video transmission signals.
Operating Frequency	2.4000-2.4835 GHz 5.150-5.250 GHz (CE: 5.170-5.250 GHz) 5.725-5.850 GHz In some countries and regions, the 5.1 and 5.8GHz frequencies are prohibited, or the 5.1GHz frequency is only allowed for indoor use. Please refer to local laws and regulations.
Transmitter Power (EIRP)	2.4 GHz: <33 dBm (FCC), <20 dBm (CE/SRRC/MIC) 5.1 GHz: <23 dBm (CE) 5.8 GHz: <33 dBm (FCC), <30 dBm (SRRC), <14 dBm (CE)
Battery
Model	TB51 Intelligent Battery
Capacity	4280 mAh
Nominal Voltage	23.1 V
Type	Li-ion
Chemical System	LiCoO2
Energy	98.8 Wh
Weight	Approx. 470 g
Operating Temperature	-20 Deg. to 40 Deg. C (-4 Deg. to 104 Deg. F)
Charging Temperature	-20 Deg. to 40 Deg. C (-4 Deg. to 104 Deg. F) If the temperature of the battery is lower than 10 Deg. C (50 Deg. F), the battery will trigger an auto-heating function. Charging in a low-temperature environment below 0 Deg. C (32 Deg. F) may shorten battery life.
Max Charging Power	205.5 W
Wired Outputs	Not supported
Battery Charging Hub
Input	100-240 V AC, max 8 A
Output	26.4 V, 7.8 A
Wireless Networking	476 W, including 65W PD fast charging of USB-C port
Security	Fast Mode: Approx. 35 minutes to 90% Standard Mode: Approx. 55 minutes to 100% Silent Mode: Approx. 80 minutes to 100% Tested at a room temperature of 25 Deg. C (77 Deg. F) and in a well-ventilated environment. In Fast mode, each battery pair is charged to 90% in sequence, and then eight batteries are charged together to 100%.
Angular Vibration Range	-20 Deg. to 40 Deg. C (-4 Deg. to 104 Deg. F)
User Controllable Range	Approx. 1,680 g
VT300-Z and VT300-L Sensor Packages
Mechanical Range	DJI PROSSD 1TB
Sensing
Forward	Measurement Range: 1.5-48 m Effective Sensing Speed: <=15 m/s FOV: Horizontal 90 Deg., Vertical 103 Deg. (landing gear raised) Horizontal 72 Deg., Vertical 103 Deg. (landing gear lowered)
Backward	Measurement Range: 1.5-48 m Effective Sensing Speed: <=15 m/s FOV: Horizontal 90 Deg., Vertical 103 Deg.
Lateral	Measurement Range: 1.5-42 m Effective Sensing Speed: <=15 m/s FOV: Horizontal 90 Deg., Vertical 85 Deg.
Upward	Measurement Range: 0.2-13 m Effective Sensing Speed: <=6 m/s FOV: Front and Back 100 Deg., Left and Right 90 Deg.
Downward	Measurement Range: 0.3-18 m Effective Sensing Speed: <=6 m/s FOV: Front and Back 130 Deg., Left and Right 160 Deg.
Operating Environment	Forward, Backward, Left, Right, and Upward: surfaces with discernible patterns and adequate lighting (lux >15) Downward: surfaces with discernible patterns and diffuse reflectivity >20% (e.g., walls, trees, people); adequate lighting (lux >15) Obstacle sensing is disabled while the landing gear is in the process of being raised or lowered.
Sensor	0-10 m
Remote Controller
Model	RM700B
Operating Time[5]	Built-in Batteries: approx. 3.3 hours Built-in Batteries Plus External Battery: approx. 6 hours
Operating Frequency	2.4000-2.4835 GHz 5.725 GHz-5.850 GHz In some countries and regions, 5.1GHz and 5.8GHz frequencies are prohibited, or the 5.1GHz frequency is only allowed for indoor use. Please refer to local laws and regulations.
Video Output Port	HDMI
Power Supply	Built-in batteries or external battery
Diagonal Field of View	Supports dual controls and coordination between multiple operators
Power Consumption	12.5 W
Operating Temperature	-20 Deg. to 50 Deg.C (-4 Deg. to 122 Deg. F)
Storage Temperature	-30 Deg. to 45 Deg. C (-22 Deg. to 113 Deg. F) (within one month) -30 Deg. to 35 Deg. C (-22 Deg. to 95 Deg. F) (one to three months) -30 Deg. to 30 Deg. C (-22 Deg. to 86 Deg. F) (three months to one year)
Battery	Built-in Battery: 3250mAh-7.2V (a set) External Battery: WB37 Intelligent Battery
Wi-Fi Protocol	Wi-Fi 6
Wi-Fi Operating Frequency	2.4000-2.4835 GHz 5.150-5.250 GHz 5.725-5.850 GHz
Focal Length	2.4 GHz: <26 dBm (FCC), <20 dBm (CE/SRRC/MIC) 5.1 GHz: <26 dBm (FCC), <23 dBm (CE/SRRC/MIC) 5.8 GHz: <26 dBm (FCC/SRRC), <14 dBm (CE)
Bluetooth Protocol	Bluetooth 5.1
Bluetooth Operating Frequency	2.4000-2.4835 GHz
Aperture	< 10 dBm
APP
Focus	DJI Pilot 2
FPV Camera
FOV	161 Deg.
Resolution	1920 x 1080@60fps

Data source: https://www.dji.com/uk/inspire-3/specs

Generated using dronespec.info
Source data acquired 2023-07-15 07:03:43