SPACECRAFT DEVICE INITIATION SYSTEM

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...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Boucher Craig, Novotney David, Kaczynski Geoff
Format:	Patent
Sprache:	eng
Schlagworte:	AIRCRAFT AVIATION CONTROL OR REGULATING SYSTEMS IN GENERAL CONTROLLING COSMONAUTICS FUNCTIONAL ELEMENTS OF SUCH SYSTEMS MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS PERFORMING OPERATIONS PHYSICS REGULATING SYSTEMS FOR REGULATING ELECTRIC OR MAGNETIC VARIABLES TRANSPORTING VEHICLES OR EQUIPMENT THEREFOR
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