Electro-optical infrared window for hypersonic applications

A guidance system for a missile performs a method for guiding the missile. The guidance system includes a target detector and a window between a target and the target detector. The window including a first pane, a second pane and a channel between the first pane from the second pane. Radiation from...

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Bibliographische Detailangaben
Hauptverfasser:	Fleder, Charles Edward, Gentilman, Richard L, Woolf, Martin A
Format:	Patent
Sprache:	eng
Schlagworte:	AIMING BLASTING COLORIMETRY HEATING LIGHTING MEASUREMENT OF INTENSITY, VELOCITY, SPECTRAL CONTENT,POLARISATION, PHASE OR PULSE CHARACTERISTICS OF INFRA-RED,VISIBLE OR ULTRA-VIOLET LIGHT MEASURING MECHANICAL ENGINEERING PHYSICS RADIATION PYROMETRY TESTING WEAPON SIGHTS WEAPONS
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Beschreibung
Zusammenfassung:	A guidance system for a missile performs a method for guiding the missile. The guidance system includes a target detector and a window between a target and the target detector. The window including a first pane, a second pane and a channel between the first pane from the second pane. Radiation from the target passes through the window including the first pane, the second pane and the channel to be detected at the target detector. A gas is transported through the channel between the first pane and the second pane to control a temperature of the window.