Test mechanism unit, and vibration test system and method under engine follow-up thrust

The invention discloses a test mechanism unit which is used for simulating follow-up thrust generated in the flying process of a slender missile. Wherein the slender missile model comprises an aluminum bar and a test engine; in an initial state, the side columns are connected with the second end of...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	CUI WEI, QIAN MING, LIU XIAOCHEN, WANG FEI, MAO KANKANG, QIANG KEJIE, ZHAO ZHIRU, LYU PING, YUE HAO
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	MEASURING PHYSICS TESTING TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR
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