ARW1000

Ready to Fly. Ready to Conquer.

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COMPLETED MISSIONS

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TOTAL FLIGHTS

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MEAN MISSION TIME

ARW1000

OVERVIEW

TYPE	QUADCOPTER
WEIGHT	7.98 KG
SPEED	22 M/S
ENDURACE	33 MIN
RANGE	3 KM
WIND RESISTANCE	18 M/S

IMAGING SYSTEM

SIYI A8 MINI CAMERA

WEIGHT	100 G
STABILIZATION	3 AXIS GIMBAL
ZOOM	6X DIGITAL
RESOLUTION	UPTO 4K
CAMERA SENSOR	1/2.7" CMOS
VIDEO OUTPUT	HDMI, ETHERNET (RTSP)

AVIONICS SYSTEM

PIXHAWK MINI ORANGE CUBE+

PROCESSOR	STM32H7
IMUs	TRIPLE REDUNDANT
BAROMETER	DUAL REDUNDANT
SIZE	COMPACT MINI
COMPATIBILITY	ARDUPILOT / PX4
VIBRATION ISOLATION	BUILT-IN VIBRATION DAMPING

AVIONICS SYSTEM

PROPULSION SYSTEM

MOTOR	T-MOTOR MN6007 II
KV RATING	320 KV
PROPELLER	T-MOTOR NS22x6.6”
ESC	T-MOTOR FLAME 70A ESCs
PEAK CURRENT	58 Amp/MOTOR

AVIONICS SYSTEM

BATTERY PACK

TYPE	Li-Ion 6S
CAPACITY	27000 mAh
ENDURANCE	33 MIN

AVIONICS SYSTEM

HERE4 GPS MODULE

GNSS	DUAL-BAND RTK (L1 + L5)
POSITIONING	RTK-CAPABLE, CENTIMETER-LEVEL
SENSORS	MAGNETOMETER, BAROMETER
INTERFACES	CAN, I2C, UAVCAN
IMU	BUILT-IN 6-AXIS IMU

AVIONICS SYSTEM

HERELINK

DATA LINK	2.4 GHz DIGITAL LINK
RANGE	UP TO 20 KM (LOS)
TELEMETRY	MAVLINK SUPPORTED
DATA RATE	500 Kbps
VIDEO STREAMING	1080P 30FPS LOW LATENCY
OUTPUT PORTS	USB, HDMI, ETHERNET

AVIONICS SYSTEM

RC LINK

TRANSMITTER	TARANIS X9D
MODULE	R9M LONG RANGE
RECEIVER	FRSKY R9SX
RANGE	UP TO 10-15 KM (LOS)
CHANNELS	UP TO 16 CHANNELS

MECHANICAL SYSTEM

DROP MECHANISM

TYPE	RETARDED PULLEY
WINCH DRIVE	N20 1000RPM DC MOTOR
RELEASE CONTROL	EMAX ES08A SERVO + ELASTIC STRAP
MATERIAL	3D PRINTED PETG
THREAD	96 FT NYLON
DESCENT CONTROL	200Ω RESISTOR REGULATION

COMPETITION TEAM

Neel

GCS OPERATOR

Aayush

SAFETY PILOT

Bhavya

CS OPERATOR

Mantra

MECHANICAL LEAD

Het

AVIONICS ENGINEER

Vishesh

CS ENGINEER

Param

MECHANICAL ENGINEER

DEVELOPMENT TEAM

Manav

Kavya

Nishanth

Aditya

TESTING PROCESS

Use the navigation buttons to follow each step of our drone testing process.

Testing Process

Prepared For Any Challenge

Design & Simulation

Analyse It Before You Build It

Drone Flight Time Analysis

A detailed analysis of drone flight time through manual calculations to select the optimal propulsion system.

Drone PDB Designing

Explore untold stories from places far and wide.

Propulsion System

High-Thrust, Efficient, and Optimized for Endurance in SUAS 2025

Manufacturing

From Concept To Craft

Best Epoxy & Weave for UAVs

The best epoxy and weave pattern for strong, lightweight structures.

Carbon Fiber Plate Curing

Curing carbon fiber plates for high-performance UAVs: process and key factors.

Stability Testing

Engineered For Balance

PID Tuning & Control Optimization

Combining Pilot Feedback and Data Analysis for Exceptional Flight Stability

Mechanical Stability

Achieving Precision Balance and Thrust Alignment for Optimal Flight

Imaging System

See Sharper Fly Smarter

Object Detection Model Selection

Evaluating and Deploying the Most Efficient Real-Time Detector for SUAS

Camera Selection for Imaging

Optimizing camera choice for performance, precision, and integration in aerial mission

Navigation

Precision In Every Direction

Object Localization from Aerial Imagery

Converting Pixel Coordinates to Real-World GPS Positions

Full System Testing

Every System. Fully Cleared

Full Mission Flight Testing

Simulating Real-World SUAS Tasks to Validate Complete System Performance

GALLERY