Standard Specification for Design and Construction of Lightweight Unmanned Aircraft Systems (UAS)
STANDARD published on 1.5.2024
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Designation standards: ASTM F3298-24
Publication date standards: 1.5.2024
The number of pages: 26
Approximate weight : 78 g (0.17 lbs)
Country: American technical standard
Category: Technical standards ASTM
This specification establishes the airworthiness requirements for the design of fixed-wing unmanned aircraft systems. It defines the baseline design, construction, and verification requirements for an unmanned aircraft system (UAS), defined as a system composed of the unmanned aircraft and all required on-board subsystems, payload, control station, other required off-board subsystems, any required launch and recovery equipment, all required crew members, and command and control (C2) links between UA and the control station. This specification applies to fixed wing UAS with permission to operate over a defined area and in airspace authorized by a nation´s civil aviation authority (CAA) with a fully interactive ground-based person as "Remote Pilot in Command."
Keywords:
UA, UAS, unmanned aircraft, unmanned aircraft system,, ICS Number Code 49.020 (Aircraft and space vehicles in general)