GJB 5107A-2019 in English
VALIDSpecification for space high-energy electron detector
- Issued on:2019-12-08
- Implemented on:2020-01-01
- File Format:PDF
- Delivery:Via email within 1~3 business days
$214.00
Introduction
Standard Evolution and Technology Upgrade
| Technical Indicators | GJB 5107-2004 | GJB 5107A-2019 | Upgrade Points |
|---|---|---|---|
| Detection Energy Range | Undefined Lower Limit | >200KeV | Clear Energy Detection Threshold |
| Data Interface | Analog Output Only | Digital Output≤2kbps | Increase Digital Transmission Capability |
| Reliability index | Confidence level not specified | Confidence level 0.7 | Quantitative evaluation standard |
Analysis of core technical requirements
Detector composition
The standard stipulates that space high-energy electron detectors must include:
- ≥3 semiconductor sensor arrays
- Electronic circuit processing system (including pre/main amplifier, high-voltage circuit, etc.)
- Space-grade structural parts
Typical application: A satellite project uses a silicon PIN sensor array to achieve 200KeV-10MeV electron energy spectrum measurement with an energy channel resolution of 8 channels.
Environmental adaptability verification system
| Test items | Identification level conditions | Acceptance level conditions |
|---|---|---|
| Thermal vacuum test | -20℃~55℃/3 cycles | -15℃~50℃/1 cycle |
| Random vibration | 10.0g(25-100Hz) | 6.0g(25-100Hz) |
| Electrostatic discharge | 10kV arc discharge | |
Implementation Suggestions
- Component Selection: Give priority to radiation-resistant devices in the aerospace model catalog, with a single-particle upset threshold ≥50MeV·cm²/mg
- Process Control: Strictly implement the key process control requirements of QJ2664, and pay special attention to the airtightness of sensor packaging
- Test Verification: It is recommended to increase the on-orbit data comparison link and verify the calibration results through actual space environment data

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