GJB 5435.5-2005
Specification for unmanned aerial vehicles strength and rigidity. Part 5: Miscellaneous loads (English Version)

Standard No.
GJB 5435.5-2005
Language
Chinese, Available in English version
Release Date
2005
Published By
Military Standard of the People's Republic of China-General Armament Department
Latest
GJB 5435.5-2005
Scope
This part specifies the strength and stiffness requirements for UAVs under other loads, and the principles to be followed in order to meet these requirements. This section applies to unmanned aerial vehicles with fixed wings and adjustable fixed wings: it applies to newly developed, improved, modified or repurposed unmanned aerial vehicles. This section does not apply to micro UAVs and UCAVs.

GJB 5435.5-2005 Referenced Document

  • GJB 540.5-1988 Airborne missile strength and stiffness specifications for airborne loads
  • GJB 5435.1-2005 Specification for unmanned aerial vehicles strength and rigidity Part 1: General specification
  • GJB 5435.7-2005 Specification for unmanned aerial vehicles strength and rigidity Part 7: Vibration
  • GJB 5435.9-2005 Specification for unmanned aerial vehicles strength and rigidity Part 9: Ground tests

GJB 5435.5-2005 history

  • 2005 GJB 5435.5-2005 Specification for unmanned aerial vehicles strength and rigidity. Part 5: Miscellaneous loads
Specification for unmanned aerial vehicles strength and rigidity. Part 5: Miscellaneous loads



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