Power that follows the mission
Follow the light.
Power the skies.
Start with the wing. Explore tandem PV
as auxiliary power for lightweight aircraft.
UAV PV applications
Fixed wing · Concept explorationFollow the light.
Continue down
AI concept images · Not actual products or flight-test footage
Application directions
A vast sky.
Many different needs.
These are potential application directions. They do not imply that existing products have completed mission validation or are ready for deployment.
Mapping and inspection
For wide-area missions,
explore supporting power.
Assess space for PV auxiliary power and supporting systems against the route, payload and aircraft platform.
Discuss mission requirementsEnvironmental observation
For observation and recording,
consider the energy system.
Study the balance of energy harvesting, storage and mission loads around sensors, observation periods and actual flight conditions.
Discuss an applicationResearch and prototype validation
Validate the concept.
Then move to applications.
Use samples, integrated prototypes and test plans to assess structural fit, electrical compatibility and performance in real environments.
Explore research and development
Integration approach
From a wing
to a complete aircraft system.
UAV PV applications require the aircraft and energy system to be designed together. Cell efficiency alone cannot establish aircraft endurance or mission capability.
- 01
Wing and structure
Assess available area, added weight, surface geometry and mounting method.
- 02
Electrical systems and storage
Specify supporting systems around the controller, energy storage, mission loads and protection requirements.
- 03
Mission and validation
Performance and suitability must be validated through project testing and actual flight conditions.
Start with the requirements
Take your flight concept
to the next step.
This page presents application concepts. The aircraft and wing integration shown are not UAV products released by HIKING PV. Existing module specifications do not establish suitability for UAV use. Each solution requires dedicated design and validation.