The design considerations for a transistorized dynamic and a carbon microphone for aircraft use are described. Both units are designed to meet Federal Aviation Agency requirements. Value engineering without sacrificing reliability is emphasized.

Author: Teder, Harry
Affiliation: Acoustic Products Division, The Telex Corporation, Minneapolis, MN
JAES Volume 15 Issue 1 pp. 63-66; January 1967
Publication Date: January 1, 1967 Import into BibTeX
Permalink: https://www.aes.org/e-lib/browse.cfm?elib=1114

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