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Приложение 10. Авиационная электросвязьТом IДо мачты выносного контрольногоустройства, если необходимоЧувствительная зона10 м(33 фут)10 м(33 фут)1.7 , BW1.7 , BWОСЕВАЯЛИНИЯ ВППАзимутальнаяантеннаКРИТИЧЕСКАЯ ЗОНАДО КОНЦА ВППСм. таблицу G-12AДопустимый разбростраектории полета (0,2°)ВИД В ПЛАНЕ4,6 м(15 фут)3 x радиусзоны Френеля3°ВППАзимутальнаяантенна2°2 x радиусзоны ФренеляЕсли необходимодля защитывыносногоконтрольногоустройства200 м(656 фут)ПРОФИЛЬЗначения дляи*X мфут ( )**мфут ( )**мфут ( )***BWИЗМЕРЯЕТСЯ ПО ГОРИЗОНТАЛИ ОТАЗИМУТАЛЬНОЙ АНТЕННЫ.ИЗМЕРЯЕТСЯ ПО ВЕРТИКАЛИ ОТАЗИМУТАЛЬНОЙ АНТЕННЫ.⎯ ШИРИНА ЛУЧА.30 (100) 1,1 (3,5) 5,7 (18,6)75 (250) 2,7 (8,7) 10,5 (34,3)150 (500) 5,3 (17,5) 17,1 (56,2)225 (750) 7,5 (24,5) 23,2 (76,0)300 (1000) 8,6 (28,3) 28,9 (94,8)Где = 0,035 X х< 200 м= 2 0,06 X х> 200 м= X tg 3° + 3 0,06 хРис. G-23А. Типовые критическая и чувствительная зоны азимутальной антенны23/11/06 19/11/09ДОП G-92№ 84
Дополнение GПриложение 10. Авиационная электросвязь17 , BWПолуширина( таблица G-12E)8°Опорная точка MLSАзимутальнаяантеннаЧувствительнаязонаВПППорог ВППРис. G-23В. Типовая чувствительная зона азимутальной антенныдля защиты наведения при пробегеДОП G-92А 19/11/09№ 84
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ПОПРАВКИОб издании
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Приложение 10. Авиац
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ПРЕДИСЛОВИЕИстори
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ПредисловиеПрилож
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ГЛАВА 2. ОБЩИЕ ПОЛОЖ
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Глава 2Приложение 10
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ДОБАВЛЕНИЕ В. ТЕХНИ
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Добавление ВПрилож
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Добавление ВПравил
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