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UT54ACS04 - Hex Inverters

General Description

The UT54ACS04 and the UT54ACTS04 are hex inverters.

The circuits perform the Boolean function Y = A.

The devices are characterized over full military temperature range of -55°C to +125°C.

Key Features

  • ‰ 1.2μ CMOS - Latchup immune ‰ High speed ‰ Low power consumption ‰ Single 5 volt supply ‰ Available QML Q or V processes ‰ Flexible package - 14-pin DIP - 14-lead flatpack ‰ UT54ACS04 - SMD 5962-96516 ‰ UT54ACTS04 - SMD 5962-96517.

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Datasheet Details

Part number UT54ACS04
Manufacturer Aeroflex Circuit Technology
File Size 220.66 KB
Description Hex Inverters
Datasheet download datasheet UT54ACS04 Datasheet

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UT54ACS04E Hex Inverters
UT54ACS00 Quadruple 2-Input NAND Gates
UT54ACS00E Quadruple 2-Input NAND Gates
UT54ACS02 Quadruple 2-Input NOR Gates
UT54ACS02E Quadruple 2-Input NOR Gate
UT54ACS08 Quadruple 2-Input AND Gates
UT54ACS10 Triple 3-Input NAND Gates
UT54ACS109 Radiation-Hardened Dual J-K Flip-Flops
UT54ACS109E Dual J-K Flip-Flops
UT54ACS11 Triple 3-Input AND Gates

Full PDF Text Transcription for UT54ACS04 (Reference)

Note: Below is a high-fidelity text extraction (approx. 800 characters) for UT54ACS04. For precise diagrams, tables, and layout, please refer to the original PDF.

View original datasheet text
Standard Products UT54ACS04/UT54ACTS04 Hex Inverters Datasheet November 2010 www.aeroflex.com/logic FEATURES ‰ 1.2μ CMOS - Latchup immune ‰ High speed ‰ Low power consumption ‰ Single 5 volt supply ‰ Available QML Q or V processes ‰ Flexible package - 14-pin DIP - 14-lead flatpack ‰ UT54ACS04 - SMD 5962-96516 ‰ UT54ACTS04 - SMD 5962-96517 DESCRIPTION The UT54ACS04 and the UT54ACTS04 are hex inverters. The circuits perform the Boolean function Y = A. The devices are characterized over full military temperature range of -55°C to +125°C. FUNCTION TABLE INPUT A H L OUTPUT Y L H LOGIC SYMBOL (1) A1 (3) A2 A3 (5) A4 (9) A5 (11) A6 (13) 1 (2) Y1 (4) Y2 (6) Y3 (8) Y4 (10) Y5 (12) Y6 Note: 1. Logic symbol in accordance with ANSI/IEEE standard 91-1984 and IEC Publication 617-12.