A thrust vector control test system of large range solid rocket engine utilizing a four-point support piezoelectric dynamometer and a deflected flange structure
Release Time:2024-10-18 Hits:
Indexed by: Journal Papers
Document Code: 391834
Date of Publication: 2024-07-10
Journal: MEASUREMENT
Volume: 234
ISSN: 0263-2241
Key Words: LOAD SHARING PRINCIPLE