Electric Aircraft Charging Requirements Survey
Survey closes February 28, 2023. De-identified summary data will be shared with all survey respondents after this time. E-mail addresses, company names and aircraft model names will not be shared.
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Email *
Company name *
Aircraft model name
All responses entered below this line will contribute to the summary data made available to all survey respondents. 
Country of origin *
Continents planned to sell or operate your aircraft
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Status of your aircraft
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Which year are you expecting / have you received certification for your aircraft?
Certification category
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Airframe configuration
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Number of occupants including pilots
Capacity per charge [kWh] (energy transfer required into the battery)
Quickest time that capacity per charge is to be delivered
Battery maximum voltage [V]
Target maximum charging current [A]
Is auxiliary power required through the charging coupler?
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If yes, please provide detail around what is required (aux voltage and charging current)
1st charging coupler preference *
2nd charging coupler preference *
Why do you prefer these charging couplers for your electric aircraft? 
The following technical questions are optional
How many charging inlets does your aircraft employ?
How many batteries are charged in parallel per inlet?
What is your charging coupler locking system preference?
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Describe your locking access control requirements (e.g. should locking be done by the charging protocol alone, or lockable and unlockable by the user?)
Please provide any other technical requirements or any general comments or suggestions
A copy of your responses will be emailed to the address you provided.
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