Golden Way UAV

{{ref improve|date=September 2014}}
{|{{Infobox Aircraft Begin
|name= [[UAV]]
|image=
|caption=
}}{{Infobox Aircraft Type
| type=Fixed-wing UAV
| national origin= [[China]]
| manufacturer= Golden Way
| designer= Golden Way
| first flight=2013
| introduced=2013
| retired=
| status= In service
| primary user= [[China]]
| number built=
| developed from=
| variants with their own articles=
}}
|}
{{chinesetext}}
Golden Way UAV is a Chinese [[UAV]] developed by [[Beijing]] [http://optics-optomechanics.goldway.com.cn/ Golden Way Scientific Co. Ltd. (Golden Way, 北京欧普特科技有限公司)], a company originally in the business of optical equipment, including those used by UAVs, and the company has recently expanded its business into producing and marketing UAVs.

==UV10==
UV10 UAV was originally developed by [[Beijing]] [http://www.microfly.com.cn/ Microfly Engineering Technology Co. Ltd. (Microfly, 北京迈凯飞工程技术有限公司)] and under the agreement reached between Golden Way and Microfly, Golden Way becomes responsible of manufacturing and marketing UV10, while Microfly would concentrate on [[Microfly UAV#UV20|Microfly UV20CAM/HS/VID]] by using Golden Way’s production facility for UV10. UV10 is a fixed wing UAV in conventional layout with high [[wing configuration]] and triclycle landing gear mounted on a cylindrical fuselage with [[V-tail]]. Propulsion is provided by a two-blade propeller driven [[tractor configuration|tractor engine]] mounted in the nose. UV10 adopts modular design concept so that different engine can be adopted for different missions, such as long range of high elevation versions.<ref name="UAV">{{cite web| url=http://www.5ihangpai.com/news/gs/201.html | title=UV10 UAV | accessdate=2014 }}</ref> UV10 can either take-off conventionally by taxiing or by catapult. Specification: <ref name="UAV0">{{cite web| url=http://www.5ihangpai.com/news/gs/195.html | title=UV10 | accessdate=2014 }}</ref>
*Length (m): 1.6
*Wingspan (m): 2.4
*Height (m): 0.6
*Payload (kg): 3
*Take-off weight (kg): 16
*Endurance (hr): 3 for high elevation version, 6 for long range version
*Fuel (L): 3
*Cruise speed (km/hr): 85 – 100
*Max speed (km/hr): 115
*Ceiling (km): 3.5
*Rate of climb (m/sec): 8
*Landing speed (km/hr): 70
*Launch: catapult or taxiing
*Catapult speed (km/hr): 60
*Catapult weight (kg): 30
*Catapult size when folded (m): 1
*Catapult size when unfolded (m): 3
*Recovery: parachute
*Remote control range (km): 30
*Deployment time (min): 5
*Max wind scale allowed for operation: 6
*Propulsion: 60 cc twin cyclinder two stroke engine for high elevation version, 35 cc single cylinder four stroke engine for long endurance version.

==See also==
[[List of unmanned aerial vehicles of the People's Republic of China]]

==Reference==
{{Reflist|2}}
[[Category:Unmanned aerial vehicles]]
[[Category:Unmanned aerial vehicles of China]]
{{UAV-stub}}