ADAPTOR AND PAYLOAD-LAUNCHING ROCKET

An object is to provide an adaptor that can attenuate a vibration acting on a payload using a simple structure, and a payload launch vehicle. The adaptor (1) according to the invention controls a vibration of the payload housed in the payload launch vehicle, and is provided between the payload and a...

Ausführliche Beschreibung

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Bibliographische Detailangaben
1. Verfasser:	TOMBE, TOSHIHIRO
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIRCRAFT AVIATION BLASTING COSMONAUTICS ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING LIGHTING MEANS FOR DAMPING VIBRATION MECHANICAL ENGINEERING PERFORMING OPERATIONS SHOCK-ABSORBERS SPRINGS THERMAL INSULATION IN GENERAL TRANSPORTING VEHICLES OR EQUIPMENT THEREFOR WEAPONS
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Beschreibung
Zusammenfassung:	An object is to provide an adaptor that can attenuate a vibration acting on a payload using a simple structure, and a payload launch vehicle. The adaptor (1) according to the invention controls a vibration of the payload housed in the payload launch vehicle, and is provided between the payload and a rocket portion. The adaptor (1) includes a tube member having a double structure including an outer tube (11) and an inner tube (12); a first elastic member (21) coupled to the outer tube (11) and the inner tube (12) at one end of the tube member; and a second elastic member (22) coupled to the outer tube and the inner tube at the other end of the tube member. The adaptor (1) is linked to the payload on the inner tube side or the outer tube side on one end side of the tube member, and linked to a leading end of the rocket portion on the outer tube side or the inner tube side on the other end side of the tube member.