发明名称 Radar proximity fuze for e.g. rocket or guided missile
摘要 The radar proximity fuze has a selectively amplified Doppler signal supplied to a conventional detonation timing circuit (6) is fed also to an active rectifier (8) in an interference suppression circuit (5). A source of bias voltage (12) representing the basic threshold, and an attenuator (13) deliver their outputs via low-pass filters (10,11) to a comparator (9). The filter time constants are chosen preferably as 100 and 1 ms respectively. A Doppler level of at least 8 dB above the system threshold in echo-free space is necessary to trigger the detonation.
申请公布号 DE3148953(C1) 申请公布日期 1996.09.19
申请号 DE19813148953 申请日期 1981.12.10
申请人 TELEFUNKEN SYSTEMTECHNIK GMBH, 89079 ULM, DE 发明人 BAUMER, HANS, ING.(GRAD.), 89250 SENDEN, DE;JACOBI, WIELAND, DIPL.-PHYS., 89075 ULM, DE;KINDERMANN, KLAUS, 89075 ULM, DE;STREB, GUENTER, ING.(GRAD.), 89250 SENDEN, DE
分类号 F42C13/04;(IPC1-7):F42C13/04 主分类号 F42C13/04
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