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Lapan Surveillance UAV 05 (LSU 05)
07 Nov 2014 • Read : 3767 x ,








Specification

Outer dimensions



Span (wingspan)

:

5.5 m

Length (long)

:

4.1 m

Height (tall)

:

1:13 am




Weight and payload



MTOW

:

77 kg

Weight empty

:

31 kg

Heavy payload

:

30 kg

Heavy fuel

:

16 kg




Achievement fly



TOG (take off ground run)

:

60 m

RoC (climb rate)

:

600 ft / min

Range

:

240 miles

Endurance

:

8 h

LG (landing ground run)

:

83 m

Ceiling

:

12000 ft

Cruise altitude

:

3000 ft

Cruise speed

:

100 km / h

Type

Multipurpose lightweight unmanned aircraft (SAR, Surveillance border areas etc)

Design features

Lightweight unmanned aircraft with a focus on the observation mission, high wing configuration provides better stability coupled with the addition hedral. The wing has a sweep of 0 deg and shape taper gives a good lift distribution. Engine placement with a pusher configuration gives the front of the space shuttle is free to put payloads and sensors without interference and vibration of the propulsion system. Tail boom mounted on two provide stability. The payload is placed on the inside of the fuselage with doors opening at the top with extra to take on the bottom of the fuselage.

Full

The aircraft is controlled by a remote control system with radio signals from the ground station. Autonomous aircraft can be controlled by using an autonomous system.

Structure

The main structure is made of GFRP by using ply-wood as an amplifier with a semi-monocoque concept.

Landing gear

The main landing gear is made with the use of GFRP reinforced plywood with brake system and rubber wheels.

Front landing gear is made by using a strut configuration with a shock absorber and rubber tires.

Resources

Resources derived from aircraft piston engine with 15 hp and 28 inch propeller. For the purposes of electricity comes from batteries contained the plane.









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