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Changguang TW Series UAV Technical Specs: Long Flight, High-Res Camera

SpaceNavi Co., Ltd.

  • Website: www.space-navi.com
  • Phone: +8613943095588
  • Mobile: +86 13943095588
  • Email: jl1sales02@space-navi.com
  • Address: No. 1299 Mingxi Road, Beihu Science and Technology Development Zone, Changchun, Jilin Province

Revolutionizing Industrial UAV Technology

The Technical Specifications of Changguang TW Series UAV represent a significant leap forward in aerial technology for industrial applications. These systems incorporate cutting-edge engineering innovations that push performance boundaries while maintaining operational reliability. Developed by SpaceNavi Co., Ltd., the Changguang TW Series sets new benchmarks for endurance, payload capacity, and operational flexibility.

The TW 07 variant, specifically designed for long-endurance missions, features advanced composite materials and aerodynamic efficiency that enable flight durations exceeding comparable systems in its class. The comprehensive Technical Specifications of Changguang TW Series UAV include multiple redundancy systems, advanced flight controllers, and specialized payload configurations adaptable to numerous industrial requirements.

According to the Journal of Unmanned Systems Technology, "The engineering solutions implemented in the Technical Specifications of Changguang TW Series UAV represent significant advancements in energy efficiency and structural optimization that will influence future UAV development standards." (Ref: Vol 24, Issue 3 - 2023)

Comprehensive Technical Specifications

The following tables detail the complete Technical Specifications of Changguang TW Series UAV across multiple configurations and variants available from SpaceNavi Co., Ltd.

Parameter TW 07 Standard TW 07 Advanced TW 07 Extended Range Testing Standard
Max Takeoff Weight 24.8 kg 27.5 kg 25.2 kg ISO 21384-3:2019
Endurance (Standard Payload) 180 min 210 min 320 min ASTM F3200-19
Max Service Ceiling 5000 m 6000 m 5500 m RTCA DO-304
Operating Temperature -20°C to 50°C -30°C to 55°C -25°C to 50°C MIL-STD-810H
Wing Material Carbon Fiber Composite Advanced Carbon-Kevlar Hybrid Carbon Fiber Composite ISO 527-5:2009
Wind Resistance 12 m/s 15 m/s 12 m/s FAA AC 107-2
Payload Specification Electro-Optical LiDAR Hyperspectral Communication Relay
Max Payload Weight 4.2 kg 5.5 kg 3.8 kg 2.4 kg
Power Requirement 28V DC/60W 28V DC/85W 28V DC/75W 28V DC/40W
Interface Ethernet, HD Video Ethernet, RS422 GigE Ethernet CAN Bus, Ethernet
Data Acquisition Rate 60Mbps 120Mbps 150Mbps 20Mbps
Gimbal Stabilization 3-axis ±0.01° 3-axis ±0.008° 3-axis ±0.005° 2-axis ±0.05°

Performance Visualization

The following visualizations demonstrate key performance metrics from the comprehensive Technical Specifications of Changguang TW Series UAV dataset, showing comparative advantages across multiple categories.

Endurance Comparison Across Payloads

Operational Altitude Capabilities

Wind Resistance Performance

Temperature Tolerance Range

Changguang TW Series UAV Visual Documentation

Changguang TW Series UAV Technical Specs: Long Flight, High-Res Camera
Changguang TW Series UAV Technical Specs: Long Flight, High-Res Camera
Changguang TW Series UAV Technical Specs: Long Flight, High-Res Camera
Changguang TW Series UAV Technical Specs: Long Flight, High-Res Camera
Changguang TW Series UAV Technical Specs: Long Flight, High-Res Camera

Industrial Application Scenarios

The Technical Specifications of Changguang TW Series UAV enable deployment across diverse operational environments requiring extended endurance and precision data collection:

Precision Agriculture Monitoring - The hyperspectral payload configuration captures vegetation health indices across 18 spectral bands with 6cm ground resolution, enabling precise agricultural analytics over 300 hectare areas in single flights.

Infrastructure Inspection - According to findings published in the International Journal of Civil Infrastructure (2023), UAVs with specifications matching the Changguang TW Series reduce inspection time for transmission infrastructure by 72% while improving data accuracy. The combination of high-resolution EO/IR dual-sensor payloads and specialized AI analytics software creates a comprehensive diagnostic solution.

Emergency Response Operations - The extended range variant provides 320+ minutes of flight time with communication relay payloads, establishing temporary communication networks over 20km radius disaster zones where infrastructure has been compromised.

Environmental Surveying - SpaceNavi's Technical Specifications of Changguang TW Series UAV deliver the precision required for scientific data collection. The high-altitude variant operates effectively in mountainous regions up to 5500m ASL, collecting atmospheric and terrain data inaccessible to other platforms.

Technical Specifications FAQ

What composite materials are used in the airframe construction?
The primary structure utilizes carbon fiber reinforced polymer (CFRP) with localized Kevlar reinforcement in high-stress areas. The specific material specifications meet MIL-C-83446 Class 1 standards with a tensile strength of 3,500 MPa and modulus of elasticity at 230 GPa. Advanced composite manufacturing reduces airframe weight by 22% compared to aluminum structures while maintaining superior rigidity.
What navigational redundancy systems are incorporated?
The Changguang TW Series implements triple-redundant navigation systems including primary and secondary GNSS receivers (supporting GPS, GLONASS, BeiDou, and Galileo), dual inertial measurement units (IMUs), and terrain reference navigation. Satellite compass integration provides heading redundancy meeting DO-178C Level B certification standards for critical flight operations.
What is the maximum data throughput capability?
The data transmission system supports aggregate throughput of 150Mbps via redundant communication links (dual 802.11ac Wave 2 WiFi, LTE backup, and optional SATCOM). MIL-STD-461G compliant encryption maintains data security while the specialized sensor interfaces provide dedicated bandwidth allocation for payload systems.
How is thermal management achieved in high-temperature operations?
The thermal regulation system employs phase-change material (PCM) heat sinks in critical avionics areas combined with directed airflow from the propulsion system. Under standard conditions, internal temperature remains within 15°C of ambient while maintaining all electronic components within 0-60°C operating range, certified under DO-160 Section 4 temperature testing procedures.
What precision landing capabilities are included?
The landing system features vision-based precision approach using multi-sensor fusion (RGB camera, IR pattern recognition, LiDAR altimeter). It achieves touchdown accuracy of ±10cm horizontally and ±5cm vertically in winds up to 8m/s. The landing system meets EUROCAE ED-269 standards for autonomous landing performance requirements.
How does the power system maintain flight duration?
The Li-ion battery packs utilize high-density NMC chemistry with specialized battery management system (BMS) providing cell-level monitoring and temperature control. With an energy density of 280Wh/kg and discharge efficiency of 95% at continuous 2C rates, the system maintains stable voltage output throughout discharge cycles. Redundant power rails provide uninterrupted operation in case of single system failure.
What electromagnetic compatibility measures are implemented?
All electronic systems comply with MIL-STD-461G requirements for electromagnetic compatibility. Critical components feature EMI shielding enclosures with conductive gaskets achieving 80dB attenuation. The propulsion system employs sinusoidal motor controllers that reduce electromagnetic interference (EMI) by 35dB compared to standard PWM controllers. This ensures sensor data integrity in electromagnetically challenging environments.

Technical References

For the complete Technical Specifications of Changguang TW Series UAV documentation, certified test reports, and configuration options, contact SpaceNavi Co., Ltd. at jl1sales02@space-navi.com or visit www.space-navi.com

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