Design Requirements for Unmanned Rotorcraft Used in Low-Risk Concepts of Operation
Design Requirements for Unmanned Rotorcraft Used in Low-Risk Concepts of Operation
- New search for: K. J. Hayhurst
- New search for: J. M. Maddalon
- New search for: N. A. Neogi
- New search for: H. A. Verstynen
- New search for: K. J. Hayhurst
- New search for: J. M. Maddalon
- New search for: N. A. Neogi
- New search for: H. A. Verstynen
This technical report presents the results of the second of two research studies on design and performance requirements supporting airworthiness certification of midrange unmanned aircraft systems (UAS) intended for commercial use. The two studies focused attention on UAS in the middle of the multidimensional spectrum of UAS; that is, UAS with attributes and capabilities exceeding the criteria to operate under Part 107 of the Federal Aviation Regulations (FARs), but without the design or operational capabilities to comply with the airworthiness standards for commercially-operated manned aircraft. The goal of the two studies was to help address the gap in airworthiness standards for some UAS that fall between the extremes.
Document information
Design Requirements for Unmanned Rotorcraft Used in Low-Risk Concepts of Operation
2016
106 pages
Report
No indication
English
Aircraft , Test Facilities & Equipment , Aircraft performance , Autonomy , Flight characteristics , Functional design specifications , Risk assessment , Rotary wing aircraft , Structural stability , Unmanned aircraft systems , Flight operations , Aircraft control , Aircraft reliability , Aircraft stability , Cargo aircraft , Commercial aircraft , Certification , Delivery , Operational hazards , Electric power plants
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