GB/T 42044-2022 in English
VALIDGeneral design requirements for utilization payloads of space station
- Issued on:2022-10-12
- Implemented on:2022-10-12
- File Format:PDF
- Delivery:Via email within 1~3 business days
$243.00
《GB/T 42044-2022空间站应用有效载荷通用设计要求》由TC570(全国载人航天标准化技术委员会)归口,主管部门为中央军委装备发展部。
Introduction
Analysis of core design requirements
Specification classification and interface adaptation
Space station payloads are divided into six categories, including SPU laboratory cabinet standard unit, SDU guide rail installation device, etc., forming a clearly subdivided standard system according to the installation location:
| Payload type | Core size (mm) | Upper mass limit (kg) |
|---|---|---|
| SPU 4x unit | 460×545×555.5 | 130 |
| SDU II type | 440×600×502 | 85.5 |
| Medium-sized standard outboard | ≤600×600×500 | Dynamic accounting |
Key technical indicators comparison
The core number supervision strategy adopts three-level redundancy management:
- Power supply module: dual topology to ensure 100% fault tolerance coverage
- Moving parts: Power ratio coefficient ≥3 to resist extreme environments
- Electromagnetic isolation: The isolation impedance of the same power supply loop is strictly ≥1MΩ
Validation process innovation
- Shock spectrum during single-machine stress verification covers 120% of the design envelope
- Full-load vacuum thermal cycle adopts a gradient of -40°C/70°C for a harsh test
- Extravehicular nuclear irradiation equivalent test exceeds the standard 12-hour continuous peak

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