Flight platform
| Type of UAV | Pure electric vertical take-off and landing composite wing |
| Pneumatic layout | Duck wing layout |
| Dynamic redundancy distribution | 8 lift motors and lift paddles / 1 tail push motor and tail push paddlesWhen the diagonal lift motor or lift propeller fails, it can hover normally |
| Dimension | 6*3.2*0.6 m |
| Empty weight | 29 kg |
| Maximum take-off weight | 68 kg |
| Maximum load weight | 15kg (two large batteries) |
| (Low altitude region) | 20kg (one large battery + one small battery) |
| Maximum speed of rise (vertical state) | 3 m/s |
| Maximum rate of descent (vertical state) | 2 m/s |
| Typical speed of ascent | 2.5 m/s |
| Maximum speed of descent | 5 m/s |
| Typical cruising speed | 25 m/s (90 km/h) |
| Maximum cruising speed | 34.8 m/s (125 km/h) |
| Typical turning radius | 200 m |
| Maximum take-off altitude | 4500 m |
| ceiling | 6000 m |
| Maximum wind resistance rating | Horizontal flight level 7 /Vertical takeoff level 6 |
| Resistance to inclement weather | Light rain / Light snow / Fog |
| Normal operating temperature range | -20~60℃ |
| The body material | 95% carbon fiber composite5% glass fiber composite material |
| Hover stability | Vertical ±1-2 mHorizontal ±1-2 m |
| The size of the landing area is required | 10*10 m |
| Landing precision | Standard configuration 2-3 metersRTK configuration 0.5 meters |
| Range of GPR | 50 m effective range |
| Maximum sailing hours per sortie | With 10kg : 3 hours + |
| (Low altitudes region) | With 15 kg : 2.5 hours + |
| Within 1 kg : nearly 6 hours | |
| Maximum range per sortie | 500 km |
Navigation and flight control
| Navigation | GNSS+INS |
| Navigation lights | Optional |
| Inertial navigation | 3 sets |
| Magnetic compass and orientation | 1 set magnetic compass / 1 set dual GNSS antennas |
| AHRS | After loss of GNSS signal, normal flight is possible for 5 minutes |
| Airplane mode | Full automatic / Semi-automatic |
| Security policy | One key return / Digital signal loss return / Low power return / Large dip Angle abnormal attitude return / Key sensor abnormal return / Vertical motor can withstand up to 2 simultaneous failure / Can also glide after the failure of the tail-thrust motor |
| Flight record | Yes |
Power system
| Motor | Brushless motor |
| Electrically controlled | FOC electrically controlled |
| Dynamic paddle | Hang a 30-inch pure carbon fiber paddle Tail push 24 inch pure carbon fiber paddle |
| IP rating | IP55 |
| Battery | 14S lithium polymer high performance battery2 or 3 blocks can be selected according to the load |
| Battery capacity | Single 61500mAh/ 11.8kg |
| Charger | Quick charge, Single block charging time 2 hours |
Data Transmission
| Digital frequency | 840-845MHz/902-928MHz Optional |
| Transmission distance | Max 150km |
Integrated figure and number (Optional)
| Figure number integrated frequency | 1427.9-1447.9MHz |
| Model | TDMA / 5 time slot Digital or graphic signals can be distributed on demand |
| Modulation | OFDM/QPSK/16QAM/64QAM |
| Antenna | Two antennasSingle transmission Double reception |
| Encryption | AES 128 |
| Transmission distance | 30 km version100 km + versionFull vision + high gain directional antenna + low EMI environment + flight to take-off altitude over km |
Packing and Installation
| Transport box size | 3*1.65*0.8 m |
| Structure | Can be disassembled into parts |
| Installation time | Takes about five minutes for two people |