CONTROL OVER SPACECRAFT HARDWARE HEATERS

FIELD: aircraft engineering.SUBSTANCE: claimed control device comprises the following components interconnected via internal trunk: microprocessor, RAM with digital data output ports, ROM and discrete data receiver port. ROM stores software of temperature setting for every setting and operation of t...

Ausführliche Beschreibung

Bibliographische Detailangaben

1. Verfasser:	GLUKHOV VITALIJ IVANOVICH
Format:	Patent
Sprache:	eng ; rus
Schlagworte:	CONTROLLING PHYSICS REGULATING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!