GB/T 38024-2019
ActiveInterface requirement for micro-nano satellite equipment
微纳卫星产品接口要求
Application Summary AI generated
This standard specifies the mechanical, electrical, thermal, and data interface requirements for equipment used in micro-nano satellites (typically under 100 kg). It is applied during the design, integration, and testing phases of small satellite development to ensure compatibility and interchangeability between different subsystems and payloads from various manufacturers. The standard facilitates modular assembly and reduces integration risks in commercial, scientific, and educational satellite projects.
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.