High-altitude UAS (thin-air, cold operation)
Unmanned aircraft engineered for thin air and extreme cold — reduced rotor/propeller thrust, cold-degraded battery capacity and cold-qualified electronics set the design limits. Mapped in the Techadyant High-Altitude Defence Atlas.
Relationships
- related toDRDO high-altitude logistics drone programme (20 kg)— DRDO high-altitude logistics UAS development programme.
- related toHIM-DRONE-A-THON (Indian Army high-altitude drone demonstrations)— Demonstration venue for high-altitude UAS (4,000–5,000 m).
- researchesIIT Jodhpur— DRDO DIA-CoE IIT Jodhpur lists drones for high-altitude mountain areas as a research thrust.
- DevelopsideaForge Technology Limited— YETI: 6,500 m maximum take-off altitude, 50–200 kg payload (company product page).
- DevelopsEndureAir Systems— SABAL described for high-altitude logistics (company).
- DevelopsBonV Aero— Air Hans: 16,500 ft operational ceiling, designed for high-altitude environments (company).
- DevelopsNavisys Technologies— Company reports high-altitude UAV trial activity.
- related toMistral Solutions— Harsh-environment embedded electronics and defence engineering (AXISCADES group).
- Depends onHigh-energy Li-ion cells— Cold degrades cell capacity; DRDO lists high-altitude battery performance and thermal management as a research need.
- related toSmall UAV (multirotor)— High-altitude variant class of small multirotor UAS.
Is anything missing on this entity?