Military Standard of the People's Republic of China-General Armament Department
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GJB 5435.7-2005
Scope
This part specifies the design requirements for structural vibration of UAVs, and the principles to be followed in order to achieve these requirements. This section applies to unmanned aerial vehicles with fixed wings and adjustable fixed wings: applicable to newly developed, improved, modified or repurposed unmanned aerial vehicles. This section does not apply to micro UAVs and UCAVs.
GJB 5435.7-2005 Referenced Document
GJB 5435.11-2005 Specification for unmanned aerial vehicles strength and rigidity Part 11: Documents and reports
GJB 5435.8-2005 Specification for unmanned aerial vehicles strength and rigidity Part 8: Aeroelastic instabilities
GJB 5435.7-2005 history
2005GJB 5435.7-2005 Specification for unmanned aerial vehicles strength and rigidity Part 7: Vibration