RJX1 and PT1 airframes


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





RJX1

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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

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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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Comments

  • Really? That's 300g/dm2. And I have concerns about 90g/dm2 on my uav project....
  • That's nothing - I've flown over 100oz/sq. ft.
  • 380cm wing span and 38Kg MTOW? If I assume a mean root chord of 50cm then I have a wing load of about 200g/dm2. Isn't that a bit too much or I'm missing something? This plane should come down like a stone...
This reply was deleted.