Rapid calculation system for pulse residual impulses of liquid-propellant rocket engine

The invention provides a rapid calculation system for the pulse residual impulses of a liquid-propellant rocket engine. The rapid calculation system comprises a data collecting device, a power supply device, a combustion chamber pressure indicating switch, a valve current indicating switch, a pulse...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	DING BOSHEN, CAO CHUN, LI ZHIGANG, YU TAO, WANG CHENGGANG, MA JUNQIANG, ZHANG WEI, CHEN FENG, GENG WEIGUO, GUAN LI, LING SIRUI
Format:	Patent
Sprache:	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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