Research Article
Designing an Efficient Emergency Response Airborne Mapping System with Multiple Sensors
| Parameters | Range |
| Length | 6.08 m | Wing span | 10.0 m | Height | 2.34 m | Engine | One ROTAX 914F | Combat radius | 250 km (in the condition of LOS indivisibility) | Service ceiling | 7000 m | Maximum level flight speed | 230 km/h | Cruise speed maximum endurance: 12 h | 150 km/h–200 km/h | Takeoff weight | ≤750 kg | Equipment weight | ≤75 kg | Working temperature | −40°C to +55°C | Relative humidity | ≤95% ± 3% | Working frequency | C band (main), UHF band (backup) | Downlink combined data transmission rate | 2 Mbps/256 Kbps | Wind against capability | Normal operation under wind of grade | Positioning error | Slant distance × 5% | Aviation transponder | Installed |
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