GB/T 40538-2021
ActiveStructural stiffness control requirements of space vehicle
空间飞行器结构刚度控制要求
Application Summary AI generated
This standard specifies the stiffness control requirements for space vehicle structures, including design, analysis, and verification methods to ensure structural stability and performance during launch and in-orbit operations. It is applied in the aerospace industry for the development and testing of satellites, spacecraft, and other orbital vehicles, particularly to prevent resonance with launch vehicle dynamics and maintain alignment of sensitive payloads.
Related Standards
GB/T 14410.11-2026
Flight dynamics—Concepts, quantities and symbols—Part 11:Control system
GB/Z 31478-2015
Process management for avionics —Preparation of an electronic components management plan
GB/Z 31477-2015
Process management for avionics-defining and performing highly accelerated tests in aerospace systems-application guide
GB/Z 44002-2024
Space environment—Method of the solar energetic protons fluences and peak fluxes determination
GB/Z 127.1-2025
Process management for avionics—Aerospace qualified electronic components (AQEC)—Part 1：Integrated circuits and discrete semiconductors
GB/T 16992-1997
Aircraft--Identification of servicing，maintenance，ground handling and safety/hazard points
GB/T 16638.2-1996
Aerodynamics--Concepts，quantities and symbols--Part 2--Axis systems and aircraft motion state quantities
GB/T 16638.1-1996
Aerodynamics--Concepts，quantities and symbols--Part 1--Aerodynamic terms in common use
Transparency note: The application summary and key sentences on this page were automatically generated by AI from the standard's original text. This content has not been human-verified and should not be used for compliance or regulatory purposes. Always refer to the official standard document from the issuing authority.