CD-20 Airplane Information and Technical Specification

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CD-20 Unmanned machine system with tube-type launch or double-launch launch method, descent and recovery. system

Preparation for the Japanese flight is only available at the time of demand, after the flight is completed.

Recovery, system removal simple, new heavy equipment release gun, ready to use, mature equipment operator available

Completely complete and complete removal within the box.

Protection arrangements for unexpected circumstances during the flight process:

Low electric power, fast oil flow;

Change in appearance:

Highly different permanent protection;

GPS localization accuracy low protection:

Combined navigation system failure protection;

Excessive maximum control radius protection;

Super departure line safety protection;

Communication interruption super time protection;

Possible location of 100 points, automatic near fall due to emergency protection situation;

Implementation of protective measures such as voluntary return, voluntary opening, voluntary descent, etc.

CD20 Unmanned machine system technical specifications:

Name	Speacification	Name	Speacification
Total length	1600mm	Maximum launch weight	17Kg
Tsubasa exhibition	Front wing: 1750mm Back wing: 1400mm	Raising and lowering method	Tube type ejection
Leveling altitude	300mm	Cruising speed	28m/s
Maximum load	5Kg	Maximum sailing time	3h
Maximum rectification rate	4m/s	Flying model	manual flight, autonomous flight
Maximum working altitude	sea level 5000m	Maximum wind resistance	6 levels

Systematic technology key points:

Self-distribution of self-opening flight lines, various designations for various points in Kanazawa area.
Improving the rapid generation of light and distance, number of navigation, proportionate scale, weight rate, etc.
The flight report was posted;

Portable ground control station with delivery service or electronic recorder, available control system communication connection free of charge.
The number of hours of operation can be controlled without human control.
Achievement of work;

The aircraft's ability to resist wind is strong, and its ability to operate under 6 different wind conditions;

Unique rapid folding structure for parts such as system fittings, etc., possible folding for each part of the system.
Rear-release projectile, non-demand tool.