GJB 5435.1-2005
GJB-Z · 2005-06-28
Specification for unmanned aerial vehicles strength and rigidity Part 1: General specification
Cited by 5
1Key Takeaways
This part specifies the structural strength and stiffness design requirements for UAVs, as well as the principles to be followed in order to achieve these requirements. This part applies to unmanned aerial vehicles with fixed wings and adjustable fixed wings: applicable to newly developed, improved, modified or repurpo…
2Scope / Description
This part specifies the structural strength and stiffness design requirements for UAVs, as well as the principles to be followed in order to achieve these requirements. This part 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 non-entry fighters.
3Version History
GJB 5435.1-2005
2005-06-28
5Citation Network
5
Cite this standard
15
Referenced herein
Standards that cite GJB 5435.1-2005
Specification for unmanned aerial vehicles strength and rigidity Part 2: Flight loads
Specification for unmanned aerial vehicles strength and rigidity Part 3: Ground loads
Specification for unmanned aerial vehicles strength and rigidity. Part 5: Miscellaneous loads
Specification for unmanned aerial vehicles strength and rigidity Part 9: Ground tests
Specification for unmanned aerial vehicles strength and rigidity Part 11: Documents and reports
Referenced by GJB 5435.1-2005
GB 3100-1993
GB 3101-1993
GB/T 3102.1-1993
GB/T 3102.10-1993
GB/T 3102.11-1993
GB/T 3102.12-1993
GB/T 3102.13-1993
GB/T 3102.2-1993
6Frequently Asked Questions
What is GJB 5435.1-2005?
GJB 5435.1-2005 — Specification for unmanned aerial vehicles strength and rigidity Part 1: General specification is an international standard developed by Military Standard of the People's Republic of China-General Armament Department. This part specifies the structural strength and stiffness design requirements for UAVs, as well as the principles to be followed in order to achieve these requirements. This part applies to unmanned aerial vehicles with fixed wings and adjustable...
What does GJB 5435.1-2005 cover?
This standard covers: This part specifies the structural strength and stiffness design requirements for UAVs, as well as the principles to be followed in order to achieve these requirements. This part applies to unmanned aerial vehicles with fixed wings and adjustable fixed wings: applicable to newly developed,...
Who should use this standard?
This standard is intended for organizations, professionals, and stakeholders involved in various industries and sectors. It is applicable to manufacturers, service providers, regulatory bodies, and certification organizations.
What is the latest version of GJB 5435.1-2005?
The current published version is GJB 5435.1-2005, published on 2005-06-28. Always check for amendments or pending revisions.
How do I purchase GJB 5435.1-2005?
You can purchase GJB 5435.1-2005 by visiting our contact page. Click "Get This Standard" to view pricing and send a purchase inquiry. Our team will respond with payment and delivery details.