- Specifications
- See also
- References
- External links
| name = Pegaz 011 | image = UAV_Pegaz.jpg | caption = }}{{Infobox aircraft type | type = Medium-range UAV for day and night reconnaissance | manufacturer = Military Technical Institute Serbia | designer = | first flight = October 2011 | introduced = | retired = | status = In development | primary user = Serbian Air Force | more users = | produced = | number built = 3 | program cost = | unit cost = | developed from = 2010 | variants with their own articles = | developed into =
}} |
The PEGAZ 011 ({{lang-sr|Пегаз}}; "pegasus") is a medium-range tactical UAV for day and night attack (armed variant),[1] reconnaissance and surveillance missions, target acquisition and designation that is being developed by Military Technical Institute in Serbia. Its flight autonomy is over 12 hours, and it sends data from the height of 3,000 m. Powered by a two-cylinder boxer type of engine with 32 kW (43 HP), it reaches the maximum flight speed of 200 km/h. The PEGAZ has a maximum weight of 230 kg, including about 40 kg of reconnaissance/surveillance equipment. It is 5.4 m long with a wingspan of 6.34 m. It takes off automatically from improvised runways and performs tasks along pre-programmed flight (optional: catapult). There are two hardpoints for optional air-to-surface missiles for attack variant. - [https://www.youtube.com/watch?v=0urB1FuB4Os Pegaz 011 Medium UAV flight video]
Specifications{{Aircraft specifications
|ref= MTI Pegaz project page[2]
|crew=none on-board
|length main=5.4 m
|length alt=17.71 ft
|span main=6.34 m
|span alt=20.8 ft
|height main=1.6 m
|height alt=5.8 ft
|area main=4.24 m2
|area alt=45.64 sq ft
|airfoil=
|empty weight main=120 kg
|empty weight alt=264 lb
|loaded weight main=40 kg
|loaded weight alt=88 lb
|max takeoff weight main=230 kg
|max takeoff weight alt=507 lb
|endurance=12 h
|engine (prop)=
|type of prop=Two cylinders boxer
|number of props=1
|power main=32 КW
|power alt=43 hp
|power original=
|max speed main=200 km/h
|max speed alt=124 mph
|cruise speed main=130-150 km/h
|cruise speed alt=81–93 mph
|stall speed main=
|stall speed alt=
|stall speed more=
|never exceed speed main=
|never exceed speed alt=
|range main= 100 km
|range alt= 62 mi
|range more=
|ceiling main=3000 m
|alt=9842 ft
|climb rate main=
|climb rate alt=
|loading main=
|loading alt=
|thrust/weight=
|power/mass main=
|power/mass alt=
|armament=
|avionics=
- Automatic takeoff from prepared runway (optional: catapult)
- Automatic landing on prepared runway (emergency: parachute)
- Fully autonomous way points tracking, holding, camera guiding Emergency and return home mode Altitude and velocity autopilot
}}See also{{aircontent
|see also=
|related=
|similar aircraft=- High Speed Target Drone
- IAI Scout
- AAI RQ-2 Pioneer
- AAI RQ-7 Shadow
- IAI Searcher
- Tadiran Mastiff
- Bayraktar PT1
- SELEX Galileo Falco
- Watchkeeper WK450
- SAGEM Sperwer
|lists=
}}References1. ^http://www.ekapija.com/website/sr/page/1407729/Vojska-Srbije-dobija-modernizovane-bombardere-orao-Pri-kraju-razvoj-bespilotnih-dronova-pegaz-i-vrabac
2. ^{{cite web|url=http://www.vti.mod.gov.rs/index.php?view=actuality&type=projects&category=1&id=138|title=MTI Pegaz project page |publisher=MTI}}
External links{{Commons|Pegaz UAV}}- Military Technical Institute Pegaz page
- Serbian National TV raport on Pegaz maiden flight
{{Military Technical Institute Belgrade}} 3 : Unmanned aerial vehicles of Serbia|Military Technical Institute Belgrade|Unmanned military aircraft |