1 36-00-04-004 ver. 0.1.0 aeroflex microelectronics solutions - hirel UT54ACS04E hex inverters december 2014 www.aeroflex.com/logic datasheet features ? 0.6 m crh cmos process - latchup immune ? high speed ? low power consumption ? wide power supply operating range of 3.0v to 5.5v ? available qml q or v processes ? 14-lead flatpack ? UT54ACS04E - smd 5962-96516 description the UT54ACS04E and the ut54 acts04e are hex inveters. the circuit performs the boolean function y = a . the device is characterized over fu ll military temperature range of -55 c to +125 c. function table logic symbol pinout 14-lead flatpack top view logic diagram input output a y h l l h y1 y2 y3 y4 (1) a1 (5) a3 (11) a5 (13) a6 note: 1. logic symbol in accordance with ansi/ieee standard 91-1984 and iec publication 617-12. 1 (3) a2 (9) a4 (2) (10) (12) (4) (8) y5 y6 (6) v dd a6 y6 a5 y5 a4 y4 a1 y1 a2 y2 a3 y3 v ss 114 213 312 411 510 69 78 y4 y3 y1 y2 y6 y5 a4 a3 a1 a2 a6 a5
2 36-00-04-004 ver. 0.1.0 aeroflex microelectronics solutions - hirel operational environment 1 notes: 1. logic will not latchup during radiation ex posure within the limits defined in the table. 2. device storage elements are immune to seu affects. absolute maximum ratings note: 1. stresses outside the listed absolute maxi mum ratings may cause permanent damage to the device. this is a stress rating only, functional operation of the device at these or any other conditions beyond lim its indicated in the operational sections is not recommended. exposure to absolute maximum ra ting conditions for extended periods may affect device reliability. 2. per mil-std-883, method 1012.1, section 3.4.1, p d = (t j(max) - t c(max) ) / jc recommended operating conditions parameter limit units total dose 1.0e6 rads(si) seu threshold 2 108 mev-cm 2 /mg sel threshold 120 mev-cm 2 /mg neutron fluence 1.0e14 n/cm 2 symbol parameter limit units v dd supply voltage -0.3 to 7.0 v v i/o voltage any pin -0.3 to v dd + 0.3 v t stg storage temperature range -65 to +150 c t j maximum junction temperature +175 c t ls lead temperature (soldering 5 seconds) +300 c jc thermal resistance junction to case 15.5 c/w i i dc input current 10 ma p d 2 maximum package power dissipation permitted @ tc = +125 o c 3.2 w symbol parameter limit units v dd supply voltage 3.0 to 5.5 v v in input voltage any pin 0 to v dd v t c temperature range -55 to +125 c
3 36-00-04-004 ver. 0.1.0 aeroflex microelectronics solutions - hirel dc electrical characteris tics for the UT54ACS04E 7 v dd = 3.3v to 5.5v; v ss = 0v 6 , -55 c < t c < +125 c) ; symbol description condition min max unit v il low-level input voltage 1 v dd from 3.0v to 5.5v 0.3 v dd v v ih high-level input voltage 1 v dd from 3.0v to 5.5v 0.7 v dd v i in input leakage current v in = v dd or v ss -1 1 a v ol low-level output voltage 3 i ol = 100 a v dd = 3.0v to 5.5v 0.25 v v oh high-level output voltage 3 i oh = -100 a v dd from 3.0v to 5.5v v dd - 0.25 v i os1 short-circuit output current 2 ,4 v o = v dd and v ss v dd from 4.5v to 5.5v -200 +200 ma i os2 short-circuit output current 2 ,4 v o = v dd and v ss v dd from 3.0v to 3.6v -100 +100 ma i ol1 low level output current 10 v in = v dd or v ss v ol = 0.4v v dd from 4.5v to 5.5v +8 ma i ol2 low level output current 10 v in = v dd or v ss v ol = 0.4v v dd from 3.0v to 3.6v +6 ma i oh1 high level output current 10 v in = v dd or v ss v oh = v dd -0.4v v dd from 4.5v to 5.5v -8 ma i oh2 high level output current 10 v in = v dd or v ss v oh = v dd -0.4v v dd from 3.0v to 3.6v -6 ma p total1 power dissipation 2, 8, 9 c l = 50pf v dd = 4.5v to 5.5v 1.0 mw/ mhz p total2 power dissipation 2, 8, 9 c l = 50pf v dd = 3.0v to 3.6v 0.5 mw/ mhz i ddq quiescent supply current v dd = 5.5v 25 a c in input capacitance 5 ? = 1mhz v dd = 0v 15 pf
4 36-00-04-004 ver. 0.1.0 aeroflex microelectronics solutions - hirel notes: 1. functional tests are conducted in accordance with mil-std-883 with th e following input test conditions: v ih = v ih (min) + 20%, - 0%; v il = v il (max) + 0%, - 50%, as specified herein, for ttl, cmos, or schmitt compatible inputs. devices may be tested using any input voltage within the above specified range, but are guaranteed to v ih (min) and v il (max). 2. supplied as a design limit but not guaranteed or tested. 3. per mil-prf-38535, for current density 5.0e5 amps/cm 2 , the maximum product of load capac itance (per output buffer) times fre quency should no t exceed 3,765pf/ mhz. 4. not more than one output may be shorted at a time for maximum duration of one second. 5. capacitance measured for initial qualifica tion and when design changes may affect th e value. capacitance is measured between the designated terminal and v ss at frequency of 1mhz and a signal amplitude of 50 mv rms maximum. 6. maximum allowable relative shift equals 50mv. 7. for devices procured with a total ionizing dose tolerance guarantee, the post-i rradiation performance is guaranteed at 25c per mil-std-883 method 1019 condition a up to the maximum tid level procured. 8. power does not include power contri bution of any ttl output sink current. 9. power dissipation specifi ed per switching output. 10. guaranteed by characte rization, but not tested. c out output capacitance 5 ? = 1mhz v dd = 0v 15 pf
5 36-00-04-004 ver. 0.1.0 aeroflex microelectronics solutions - hirel ac electrical characteristics for the UT54ACS04E 2 (v dd = 3.0v to 5.5v; v ss = 0v 1 , -55 c < t c < +125 c); notes: 1. maximum allowable relative shift equals 50mv. 2. for devices procured with a total ionizing dose tolerance guarantee, the po st-irradiation performance is guaranteed at 25c per mil-std-883 method 1019 condition a up to the maximum tid level procured. symbol parameter condition v dd minimum maximum unit t plh input to yn c l = 50pf 4.5v to 5.5v 1 6 ns 3.0v to 3.6v 1 8 t phl input to yn c l = 50pf 4.5v to 5.5v 1 8.5 ns 3.0v to 3.6v 1 12.5
6 36-00-04-004 ver. 0.1.0 aeroflex microelectronics solutions - hirel packaging 1. all exposed metallized ar eas are gold plated over electroplated nickel per mil-prf-38535. 2. the lid is electrically connected to v ss . 3. lead finishes are in accordance with mil-prf- 38535. 4. dimension symbol is in accordance with mil- prf-38533. 5. lead position and cola narity are not measured. figure 1. 14-lead flatpack
ordering information: ut54acts04e: smd drawing number: 96516 = UT54ACS04E device type: 02 = 1 rad(si)/sec package type: x = 14-lead ceramic botto m-brazed dual-in-line flatpack lead finish: (notes 1 & 2) a = solder c = gold x = optional 5962 ***** ** * * * * total dose: (notes 3 & 4) r = 1e5 rads(si) f = 3e5 rads(si) g = 5e5 rads(si) h = 1e6 rads(si) 03 = 50 to 300 rads(si)/sec class designator: q = qml class q v = qml class v 96517 = ut54acts04e notes: 1. lead finish (a,c, or x) must be specified. 2. if an ?x? is specified when or dering, part marking will match th e lead finish and will be either ?a? (solder) or ?c? (gold). 3. total dose radiation must be specified when ordering. qml q and qml v not available without radiation hardening. for protot ype inquiries, contact factory. 4. device type 02 is only offered with a tid tolerance guarantee of 3e5 rads(si) or 1e6 rads(si) and is tested in accordance wi th mil-std-883 test method 1019 condition a and section 3.11.2. device type 03 is only offered with a tid tolera nce guarantee of 1e5 rads(si), 3e5 rads(si) , and 5e5 rads(si), and is tested in accordance with mil-std-88 3 test method 1019 condition a.
8 www.aeroflex.com info-ams@aeroflex.com our passion for performance is defined by three attributes represented by these three icons: solution-minded, performance-driven and customer-focused aeroflex colorado springs (aeroflex) reserves the right to make changes to any products and services herein at any time without notice. consult aeroflex or an authorized sales representative to verify that the information in this data sheet is current before using this product. aeroflex does not assume any responsibility or liability arising out of the application or use of any product or service described herein, except as expressly agreed to in writing by aeroflex; nor does the purchase, lease, or use of a pr oduct or service from aeroflex convey a license under any patent rights, copyrights, trademark rights, or any other of the intellectual rights of aeroflex or of third parties. this product is controlled for export under the u.s. department of commerce (doc). a license may be required prior to the expo rt of this product from the united states. aeroflex colorado springs - datasheet definition advanced datasheet - product in development preliminary datasheet - shipping prototype datasheet - shipping qml & reduced hirel
9 36-00-04-004 ver. 0.1.0 aeroflex microelectronics solutions - hirel datasheet revision history revision date description of change december 2014 version 0.1.0 initial release of advanced data sheet
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