PDF(7533 KB)
PDF(7533 KB)
PDF(7533 KB)
可重复使用火箭着陆回收机构的试验验证技术
Test and Validation Technology for Landing Recovery Mechanisms of Reusable Launch Vehicles
| {{custom_ref.label}} |
{{custom_citation.content}}
{{custom_citation.annotation}}
|
/
| 〈 |
|
〉 |