Spaceware Sky Vision II
Sky Vision (Yuan-Jian or Yuanjian, 远见) UAVs are a series of Chinese UAVs developed by [ Beijing Sky Universe Digital City Science and Technology Co., Ltd. (Spaceware, 北京天宇数字城市科技有限公司)], and some of which are manufactured by its subsidiary Ordos City China Science Flying Universe Science and Technology Co., Ltd. (鄂尔多斯市中科飞宇科技有限公司)
| UAV | |
|---|---|
| Role | UAV |
| National origin | China |
| Manufacturer | Spaceware |
| Designer | Spaceware |
| First flight | 2014 |
| Introduction | 2014 |
| Status | In service |
| Primary user | China |
Sky Vision II
As of end of 2014, all Spaceware UAV marketed is Sky Vision II series:
| Model | 1600[1] | 2700[2] | 3600[3] | 4700[4] | 7200[5] |
|---|---|---|---|---|---|
| Layout: | Tailless | Conventional | Twin boom | Twin boom | Twin boom |
| Wing configuration: | Mid | High | High | High | High |
| Empennage configuration: | Tailless | Fuselage mounted | Inverted V-tail | Twin tail | V-tail |
| Propulsion configuration: | Tractor configuration | Tractor configuration | Pusher configuration | Pusher configuration | Pusher configuration |
| Landing gear: | None | None | None | Tricycle | Tricycle |
| Length (m): | 0.98 | 1.8 | 1.8 | 2.58 | 3.795 |
| Height (m): | 0.48 | 0.47 | 0.27 | 0.912 | 1.202 |
| Wingspan (m): | 1.58 | 2.7 | 3.6 | 4.769 | 4.188 |
| Wing area (sq m): | 0.5 | 1 | 1 | 1.9 | 3 |
| Winglets: | Downward | None | None | Upward | Upward |
| Payload compartment (L): | 3 | 12 | 16 | 28 | 120 |
| Empty weight (kg): | 4 | 16 | 15 | 37 | 100 |
| Max take-off weight (kg): | 8 | 18 | 32 | 85 | 200 |
| Payload (kg): | 2 | 5 | 8.5 | 26 | 30 |
| Ceiling (km): | 4 | 6.5 | 6.5 | 6.5 | 6.5 |
| Max rate of climb (m/s): | 5 | 5 | 5 | 5 | 5 |
| Max g load: | 5 | 5 | 5 | 5 | 5 |
| Max speed (km/h): | 120 | 160 | 160 | 180 | 180 |
| Max range (km): | 100 | 450 | 480 | 600 | 1500 |
| Max endurance (h): | 1 | 3.5 | 3 | 5 | 12 |
| Cruise speed (km): | 80 | 120 | 129 | 125 | 130 |
| Cruise altitude (m): | 300 – 1000 | 300 – 1000 | 300 – 1000 | 300 – 1000 | 300 – 1000 |
| Typical range (km): | 60 | 300 | 240 | 420 | 1400 |
| Typical endurance (h): | 0.75 | 2.5 | 2 | 3.5 | 11 |
| Max wind scale for flight: | 4 | 6 | 6 | 7 | 7 |
| Max wind scale for take-off & land: | 3 | 4 | 4 | 5 | 5 |
| Fuel (L): | 6 | 6 | 8 | 13 | 72 |
| Propulsion: | Internal combustion engine | Internal combustion engine | Internal combustion engine | Internal combustion engine | Internal combustion engine |
| Fuel consumption (L/h): | 1.5 | 1.5 | 2.2 | 2.4 | 5.2 |
| Propeller: | 2 or 3 blades | 2 blades | 2 blades | 2 blades | 2 blades |
| Data transmission: | Continuous | Continuous | Continuous | Continuous | Continuous |
| Navigation: | GPS + WCDMA | GPS + WCDMA | GPS + WCDMA | GPS + WCDMA | GPS + WCDMA |
| Launch: | Hand or catapult | Catapult | Catapult | Taxiing | Taxiing |
| Recovery: | Parachute | Parachute | Parachute | Taxiing | Taxiing |
References
- "Sky Vison II 1600". Retrieved 2014. Check date values in:
|accessdate=(help) - "Sky Vison II 2700". Retrieved 2014. Check date values in:
|accessdate=(help) - "Sky Vison II 3600". Retrieved 2014. Check date values in:
|accessdate=(help) - "Sky Vison II 4700". Retrieved 2014. Check date values in:
|accessdate=(help) - "Sky Vison II 7200". Retrieved 2014. Check date values in:
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