QJ 2406A-2005 in English
VALIDRequirement and review for reliability design of solid rocket motor
- Issued on:2005-04-17
- Implemented on:2005-07-01
- File Format:PDF
- Delivery:Via email within 1~3 business days
$272.00
| Standard No: | QJ 2406A-2005 |
| Document status: | VALID |
| Title in English: | Requirement and review for reliability design of solid rocket motor |
| Title in Chinese: | 固体火箭发动机可靠性设计要求和评审 |
| Language: | English |
| File Format: | Electronic (PDF) |
| Delivery: | Via email within 1~3 business days |
| Issued on: | 2005-04-17 |
| Implemented on: | 2005-07-01 |
| ICS Classification: | 49.050-Aerospace engines and propulsion systems |
| Chinese Classification: | V72-Spacecraft power system |
| Professional Classification: | QJ-Aerospace |
| Related Keywords: | reliability design
reliability design criteria key reliability items reliability allocation reliability prediction |
| Related Topics: | rocket engine
a solid reliability design reliability design solid generator qj 3212 2005 KS 2406 qj2406 qj 2406a |
Scope
This standard specifies the main work items and review requirements such as solid rocket motor (hereinafter referred to as the engine) reliability model establishment, reliability allocation, reliability prediction, reliability design criteria, failure mode and impact analysis, key reliability items, etc. This standard applies to the reliability design and review of strategic and tactical missiles and aerospace engines.
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