| Country | United States |
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| Airframe / lift type | Multirotor – quad |
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| Control / autonomy level | Fully autonomous (human-off-the-loop, AI-navigated), Semi-autonomous (human-on-the-loop) |
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| Domain | Aerial (UAV/UAS) |
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| Mission / use case – civil | Inspection, Public safety / SAR |
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| Mission / use case – military | ISR |
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| Origin / supply chain | COTS (DJI, Autel, Skydio) |
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| Propulsion | Electric (LiPo / Li-ion) |
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| Range / endurance | Close range (5–50 km, 1–6 hrs) |
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| Signature / detectability | GNSS-denied capable, RCS – nano/micro (<0.01 m²), RF-emitting, RF-silent – optical navigation |
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| Speed regime | Medium (50–150 km/h) |
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| Threat vector | Surveillance / reconnaissance |
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| Weight / class | Class I – Mini (2–20 kg), FAA <25 kg (Part 107) |
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| Confidence | low |
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