SPACECRAFT DEVICE INITIATIONSYSTEM

SPACECRAFT DEVICE INITIATIONSYSTEM

One aspect of the present invention involves a networked initiation system having one or more non-energetic hold-down and release mechanisms ("HDRMs"), a control unit and an interface bus connected between all of the HDRMs and the control unit. Other aspects of the present invention involv...

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Hauptverfasser: KACZYNSKI, Geoff, BOUCHER, Craig, NOVOTNEY, David
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AIRCRAFT
AVIATION
COSMONAUTICS
PERFORMING OPERATIONS
TRANSPORTING
VEHICLES OR EQUIPMENT THEREFOR
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creator KACZYNSKI, Geoff
BOUCHER, Craig
NOVOTNEY, David
description One aspect of the present invention involves a networked initiation system having one or more non-energetic hold-down and release mechanisms ("HDRMs"), a control unit and an interface bus connected between all of the HDRMs and the control unit. Other aspects of the present invention involve networked initiation systems having one or more of each of non-energetic HDRMs, energetic HDRMs and other (generic) energetic devices. The systems also include a control unit and an interface bus connected between all of the HDRMs and/or energetic devices and the control unit. The system may be used on a spacecraft for holding various elements in place on the spacecraft during launch, and then activating the HDRMs and/or energetic devices at selected points in time after launch to release the elements for movement, e.g., into orbit or beyond.
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subjects AIRCRAFT
AVIATION
COSMONAUTICS
PERFORMING OPERATIONS
TRANSPORTING
VEHICLES OR EQUIPMENT THEREFOR
title SPACECRAFT DEVICE INITIATIONSYSTEM
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