ASTM F3298-24 img
Active standard | Published: 01/05/2024

ASTM F3298-24

Standard Specification for Design and Construction of Lightweight Unmanned Aircraft Systems (UAS)

Available languages: English

Available design: Online Secure PDF, Standard + Redline - Online secure PDF, Print design, Print + redline

from 104.00 USD show on eshop

Detail information

Designation: ASTM F3298-24

Publication date: 01/05/2024

Pages: 26

Country: American technical standard

Where to buy?

You can buy at www.mystandards.biz

Anotation

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)
Loading
Cookies Cookies

Potřebujeme Váš souhlas k využití jednotlivých dat, aby se Vám mimo jiné mohli ukazovat informace týkající se Vašich zájmů. Souhlas udělíte kliknutím na tlačítko „OK“.

Souhlas můžete odmítnout zde.

Zde máte možnost přizpůsobit si nastavení souborů cookies v souladu s vlastními preferencemi.

Potřebujeme Váš souhlas k využití jednotlivých dat, aby se Vám mimo jiné mohli ukazovat informace týkající se Vašich zájmů.