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ASTM F3002-22

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Standard Specification for Design of the Command and Control System for Small Unmanned Aircraft Systems (sUAS)

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1.1 This specification is provided as a consensus standard in support of an application to a nation’s governing aviation authority (GAA) for a permit to operate a small unmanned aircraft system (sUAS) for commercial or public use purposes.

1.2 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety, health, and environmental practices and determine the applicability of regulatory limitations prior to use.

1.3 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.


This specification provides a consensus standard for an application to a nation's governing aviation authority (GAA) for a permit to operate a small unmanned aircraft system (sUAS) for commercial or public use purposes. It is intended for all sUAS that are allowed to operate over a defined area and in airspace authorized by a nation's GAA. Unless otherwise specified by a nation's GAA, this specification applies only to UA that have a maximum gross takeoff weight of 25 kg (55 lb) or less. This specification covers general command and control (C2) requirements, C2 system spectrum requirements, C2 link requirements, UA requirements, and fly-away functionality.


SDO ASTM: ASTM International
Document Number F3002
Publication Date Oct. 1, 2022
Language en - English
Page Count 5
Revision Level 22
Supercedes
Committee F38.01
Publish Date Document Id Type View
Oct. 1, 2022 F3002-22 Revision
June 1, 2014 F3002-14A Revision
Jan. 15, 2014 F3002-14 Revision