The design and performance of an UAS with a maximum gross weight of 1320 pounds. The specification covers airworthiness requirements for an acceptable powered fixed wing aircraft UAS.
This standard is needed to provide airworthiness requirements of design and performance to Class 1320 powered fixed wing UAS aircraft.
KeywordsClass 1320 powered fixed wing aircraft UAS
The title and scope are in draft form and are under development within this ASTM Committee.Back to Top
Draft Under Development