Product Development Timeline
Design Strategy
ETN200
Parametric Study
Concept Design
Detail Design
Specified the aircraft requirement. The certification specification of the Special Condition Vertical Take-off and Landing Aircraft are taken into consideration in the design strategy of ETN200 as well as:
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Payload weight 200kg
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Endurance range 45km
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Vertical take-off and landing
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Autonomous control system
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Driven by electric power plant
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Safety features during loading/unloading
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Seamless integration with the current logistic operation
Perform a detailed design parametric study on the system architecture to fulfill the functional breakdown of the aircraft based on the special condition vertical take-off and landing certification specifications.
Develop a design concept based on the parametric study's outcome to deliver the specifications needed for the certification and boost its commercialization value.
Detail design with analytical analysis and simulation on the airframe and system. Generation of engineering drawing, engineering order, report, and procurements of parts and components.
Consultation with the Relevant Authority
Consult with the stakeholder of the aircraft certification such as CAAM, MCMC, JUPEM, and SIRIM to get their input and for further design progress.
Manufacturing, Laboratory Test, and Integration
Manufacture the part as required according to engineering order and engineering drawing. The system will be tested at the every stage of development to ensure its reliability.
Controlled Environment Test
Perform laboratory tests on the airframe and system to determine and verify analytical analysis on the capability, functionality, and performance of the design.
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Wind tunnel test
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Static and dynamic thrust test
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Structure test
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Battery endurance test
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Power plant test
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Energy Management test
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Motor and ESC test
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Propellers balance test
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Electrical and EMC test
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Full system test
Field Testing
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Flight control system gain tuning
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Environmental chamber test
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Emergency battery endurance test
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Structure test
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Sensor control calibration
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Full system test
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Indoor flight hover test
Special Flight Permit
To seek approval from CAAM for flight testing permit.
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Related engineering order, engineering drawing, and report
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Engineering material specification
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Master equipment list
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Minimum master equipment list
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Configuration list
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Minutes of meeting preparation
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Design acceptance strategy report
Flight Testing
To perform the mission flight test.
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Outdoor flight hover test
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Communication quality and range test
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Mission flight test
Standard Operating Procedure (SOP) and Publication
To seek approval from CAAM for flight testing.
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Operation manual
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Maintenance manual
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Flight manual
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Illustrated part catalogue
Type Certification
To seek approval from CAAM for type certification based on EASA-SC-VTOL-01 and DO 160 for aircraft certification and airworthiness.
Operation
Pre commercialization of ETN200
In cooperated widely
We will work closely with established industry leaders and local governments to help bring our ideas to reality.
