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Database: 365,228(8 Aug 2026)
devices grade b devices grade c devices quality assurance level aerospace key systems general aerospace systems discrete semiconductor devices general spacecraft systems general specification nitrophosphate-karl fischer method introduction gb damaged fuel assemblies interoperation technique requirements
GB/T 43366-2023 in English

GB/T 43366-2023 in English

VALID

General specification for discrete semiconductor devices of space application

  • Issued on:2023-11-27
  • Implemented on:2024-03-01
  • File Format:PDF
  • Delivery:Via email within 5 business days
Price(USD): $670.00
$650.00
Standard No: GB/T 43366-2023
Document status: VALID
Title in English: General specification for discrete semiconductor devices of space application
Title in Chinese: 宇航用半导体分立器件通用规范
Language: English
File Format: Electronic (PDF)
Delivery: Via email within 5 business days
Issued on: 2023-11-27
Implemented on: 2024-03-01
ICS Classification: 49.035-Components for aerospace construction
Chinese Classification: V25-Electronic components
Professional Classification: GB-National Standard
Related Keywords: devices grade b devices grade c devices quality assurance level aerospace
key systems general aerospace systems
discrete semiconductor devices
general spacecraft systems
general specification
Related Topics: aerospace
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Semiconductor Device Usage Rules
discrete device
discrete device
Semiconductor Discrete Devices
semiconductor effect
semiconductor
Specification document about navigation
Semiconductor Discrete Devices International
Total dose test method for aerospace semiconductor devices
Semiconductor device material references

《GB/T 43366-2023宇航用半导体分立器件通用规范》由TC425(全国宇航技术及其应用标准化技术委员会)归口,TC425SC2(全国宇航技术及其应用标准化技术委员会宇航电子分会)执行,主管部门为国家标准委。


Introduction

Analysis of the core framework of the standard

Technical dimensions Grade A devices Grade B devices Grade C devices
Quality assurance level Aerospace key systems General aerospace systems Non-critical loads
High temperature life test (h) 1000 340 48
Number of temperature cycles 500 25 20

Key Technical Requirements

4.2 Quality Assurance Level System

The standard establishes a three-level quality assurance system: Level A is applicable to key systems such as long-life satellites (with the highest test severity), Level B is used for general spacecraft systems, and Level C is applicable to short-term mission payloads.

  • Grade A needs to pass 1000 hours of 240℃ assessment
  • Grade B requires 160 hours of testing under the same conditions
  • Grade C only needs 48 hours of verification

4.5 Identification System Specifications

Unique seven-segment identification code:

Example: A R-IV QX-1002 means:

  1. A - Quality assurance grade A
  2. R - Total dose resistance 103Gy(Si)
  3. IV - Single event effect threshold ≥75MeV·cm2/mg
  4. QX-1002 - Device model
  5. M 30 Low Earth Orbit Satellite H 104 Deep Space Detector

    5.9 SEM inspection standards

    SEM resolution is required to be ≤10nm, and the key inspections are:

    • Metalization layer defects at the oxide layer step
    • Metal strip cross-sectional area loss rate <50%
    • Zero tolerance for unattached defects in the bonding area

    Implementation suggestions

    Supply chain management

    Outsourced chips need to be evaluated according to Table 4 for wafer batches:

    • Grade A devices must provide chip identification reports
    • 22 pieces of sampling passed the high temperature life test with zero failures
    • The change in key parameters Δ needs to be continuously monitored

    Acceptance process optimization

    It is recommended to adopt a three-level acceptance strategy:

    1. Incoming inspection: Check the integrity of the identification system
    2. DPA analysis: Destructive verification of 3-5 pieces per batch
    3. Batch release: Comprehensive judgment based on 6.5 basket selection data

Sample only — not a preview of GB/T 43366-2023
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