Spaceware Sky Vision II
UAV | |
---|---|
Role | UAV |
National origin | China |
Manufacturer | Spaceware |
Designer | Spaceware |
First flight | 2014 |
Introduction | 2014 |
Status | In service |
Primary user | China |
|
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)
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 |
See also
List of unmanned aerial vehicles of China
References
- ↑ "Sky Vison II 1600". Retrieved 2014. Check date values in:
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(help) - ↑ "Sky Vison II 2700". Retrieved 2014. Check date values in:
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(help) - ↑ "Sky Vison II 3600". Retrieved 2014. Check date values in:
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(help) - ↑ "Sky Vison II 4700". Retrieved 2014. Check date values in:
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(help) - ↑ "Sky Vison II 7200". Retrieved 2014. Check date values in:
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(help)
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