GUIDED ANTI-AIRCRAFT MISSILE

rocketry. SUBSTANCE: guided anti- aircraft missile has a detachable zero stage and a sustainer stage with a radio-command control equipment and a luminous radiator unit in the rear section of the stage. Installed in the luminous radiator unit in a luminous element is a pulse laser semiconductor radi...

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Bibliographische Detailangaben
Hauptverfasser:	MAKHONIN V.V, FILIPPOV S.A, SHABLOVSKIJ V.I, DUDKA V.D, KUZNETSOV V.M
Format:	Patent
Sprache:	eng
Schlagworte:	AMMUNITION BLASTING EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION HEATING LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	rocketry. SUBSTANCE: guided anti- aircraft missile has a detachable zero stage and a sustainer stage with a radio-command control equipment and a luminous radiator unit in the rear section of the stage. Installed in the luminous radiator unit in a luminous element is a pulse laser semiconductor radiator made in the form of a solid cylindrical heat-accumulating casing, hermetically closed by a cover with a glass outlet port. Radiating crystal diode units are installed inside the casing on the circular surface of the insulator - heat sink uniformly in the circumference in different planes and at an angle to each other. EFFECT: enhanced noise immunity of the optical communication line, reduced power consumption and overall dimensions of the optical radiator. 3 dwg