Source: http://asmaraaerospace.yolasite.com/uav-airframe.php
RJX1
Airframe Specifications
| Propulsion Specifications
Payload Allowance
|
Aircraft Performance
Stall Speed | 40kts (approx) |
Cruise Speed | 45kts (approx) |
Max Speed | 80kts |
Crosswind Takeoff/Landing | maximum 30kts crosswind |
Takeoff Distance | 50m (3kg payload) with flaps set 0deg |
Landing Distance | 30m (3kg payload) with 30deg flap |
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PT1
PT1 Specifications
Wing Span | 280cm |
Length | 200cm |
Empty Weight | 5kg |
MTOW | 9kg |
Landing Gear Configuration | Tri-cycle |
Actuators | Servos (8pieces) |
Propulsion | 45cc Modified Piston Petrol Engine |
Propeller | 20 x 10” |
Fuel Tank | 1500cc complete with rubber tubing |
Takeoff Distance | 60 – 80m |
Landing Distance | 50 – 70m |
Stall Speed | 40kts |
Cruise Speed | 50kts |
Maximum Speed | 100kts |
Minimum Banking Radius | 25m |
Endurance | 1.5 hours (approx.) |
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