Arash Joorabchi's Posts

Source: http://asmaraaerospace.yolasite.com/uav-airframe.php

RJX1

Airframe Specifications

Wing Span	380cm
Length	250cm
Empty Weight	21kg
MTOW	38kg
Airframe Material	Hybrid Composite Material
Landing Gear	Aluminium Alloy + Hardened Steel
Wheels	Rubber Compound
Control Surfaces	Aileron, Elevator, Rudder, Flaps
Servo Type	High Torque
Number of Servos	8

Propulsion Specifications

Engine	Twin Cylinder Petrol Engine
Capacity	80cc
Power	7.5bhp
Propeller	24”x10 (various pitch available)
Fuel Storage	6litres (fuselage allows 9litres)
Fuel Consumption	15ml/min (approx.)

Payload Allowance

Aft Cabin	33 litre
Forward Cabin	12 litre
Max Payload	16kg

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.)

Arash Joorabchi's Posts (2)

RJX1 and PT1 airframes

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