ADJUSTABLE ATTENUATION SYSTEM FOR A SPACE RE-ENTRY VEHICLE SEAT

An adjustable attenuation system 10 for a space re-entry vehicle seat having a frame 12 that supports at least one seat 14 mounted to and supported on the frame 12 at the seat back. A plurality of struts 16 is attached to the frame 12 in predetermined locations 18. The struts 16 are also attached, b...

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Bibliographische Detailangaben
Hauptverfasser:	SIMON XAVIER D, BARACKMAN VICTOR J
Format:	Patent
Sprache:	eng
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS PARACHUTES PERFORMING OPERATIONS TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE TRANSPORTING
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Beschreibung
Zusammenfassung:	An adjustable attenuation system 10 for a space re-entry vehicle seat having a frame 12 that supports at least one seat 14 mounted to and supported on the frame 12 at the seat back. A plurality of struts 16 is attached to the frame 12 in predetermined locations 18. The struts 16 are also attached, by way of mounting brackets 20 to predetermined locations on the spacecraft (not shown). The struts 16 are interconnected by a tubing system 22, which sets the tension of the struts 16 by way of a controller 24.