ARMY MIL-M-50747-1973 MALF 3 BUFFER LOGIC 11738803《MALF 3 型逻辑缓冲器11738803》.pdf
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1、MIL-fl-50747 12 M 7993706 0330578 2 II Y f - r- - _- MIL-M - 5 0747(MU) 8 August 1973 MILITARY SPECIFICATION MALF 3 BUFFER LOGIC: 11738803 This specification is approvelaintenance, and Disposition of Sqldering, Manual Type, High ?Pliability Electrical, Electronic, Ixstrument, Communication, and 3ada
2、r for Aerospace and Control S:;stems, Procedures for Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL- M- 50747 (MU) 8 August 1974 MIL-S-46841 Solder Bath Soldering of Printed Wiring Assemblies, Automatic Machine Type STANDARDS Military MIL-STD- 1
3、 O5 Sampling Procedures and Tables for Inspection by Attributes Quality Assurance Terms and Definitions MIL-STD-1 O” MIL-STD-83 CI Environmental Test Methods DRA WINGS U, S. A.rmy, Frail-ford Arsenal F11738803 MALF 3 Buffer Logic: 11738803 PACKAGING DATA SHEET 11738803 Packaging of MALF 3 Buffer Log
4、ic: 11 738803 (Copies of specifications, c:zndards, drawings, and packaging data sheets required by suppliers in ccrxction with specific procurement functions should be obtained from the ?rocuring activity or as directed by the contracting officer. ) Provided by IHSNot for ResaleNo reproduction or n
5、etworking permitted without license from IHS-,-,-MIL-M-50747(MU) 8 August 1973 3. REQUIREMENTS 3.1 Fabrication. The MALF 3 Buffer-Logic, herein referred to as the assembty, shali be manufactured in accordance with Drawing F11738803 and d-rawings- pertaining thereto, . 3.2 General specification. The
6、assembly shall meet the . following reqzrements, where applicable, of MIL- F- 13926: .a. Order of precedence b. Dimensions and tolerances c Part identification and marking d. Electrical and electronic assemblies e. Part ident.ification and marking f. Wo rkmanship. 3.2.1 Solde ring. Soldering shall b
7、e in accordance with MIL-S- 45743 or MIL-S-46844, except that bare copper wire exposure shall be permitted at clipped ends of component leads. 3,3 Performance. Unless otherwise specified, the assembly shall meet the performance requirements of this specification at standard ambient temperatures betw
8、een 60 degrees Fahrenheit (O F) and 90” F. . - 3.3.1 Loads, power, and signals. The assembly shall perform as specified herein when the loads, power, and signals of table I are applied as specified, . 3. 3.1 1 Reset signal, I) applied to Pl-10 as shown in figure 1, the output at Pi-29 and Pl-30 shal
9、l be as shown in figure 1. With the type-B signal (item 3. 3 of table (These signals may be recurring.) Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-M-50747(MU) 8 August 1973 Item 1. - 1.1 1.2 1 .-3 1.4 1.5 2. 2.1 3. 3.1 3.2 3.3 TABLE I LOADS,
10、 POWER, AND SIGNALS C ondit ions Loads Impedance Impedance Impedance NAND Gate NAND Gate Power Source t5 vac Signal Sources Digital Type -A Digital Type -A 1 Digital Type -B Cha ra ct e ri s tic s , 16052 k5 percent in series with 62 pf f10 percent 16052 k5 percent in series with 62 pf f10 percent 1
11、6OQ i5 percent in series with 62 pf f10 percent 1 Gate-DTpL 9946 or equivale nt 2 Gates-DTpL 9946 or e q ui val e nt Tolerance: LO.2 Vdc Ripple: - 25 mV p-p Logical one: t4. O *l. OV Sour ce impedance : 6K62 *15 percent Logical zero: to. 2 *O. 2V Pulse width and PRF as s pe c ified he re in. Logical
12、 one: t4. O rtl, OV Source impedance: 68052 I30 percent Logical zero: +O. 2 *O. 2V Pulse width and PRF as specified herein. Logical one: t4. O *l. OV Source impedance : 150 S2 I30 percent Logical zero: +O. 2 *O. 2V Pulse width and PRF as s peci fied her ein. Connections Connected between the followi
13、ng pins: Pl-30 and Pl-29 P1-I6 and P1-I7 Pl-19 and Pl-18 PI -3 and P1-7 P1-32 and P1-7 P1-5(t) and PI -7 (- 1 Applies as speci- fied herein. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-M- 50747(MU) 8 August 1973 Input to P1-10 _ - - - - - Log
14、ical one - - - - - - - - - - - Logical zero 1-4 I I 1. 0 rt. 1 psec t and t 40 nanoseconds (ns) (10 and 90 percent amplitude points) I r f- 41 - iysec - - - t3.5rt1.5v - - - - +0.4*0.4 v l I- I I O tit put f I oin i. O rt0.2 ysec I 1-4 . P1-29 I I I I I I I 1 t3.5 *l. 5 v - - - - - - - - - tO.4IO.4
15、v - Output from I I P1-30 Figiire 1. Reset Signal Waveforms 3. 3. 1.2 Range signal. With no input signal applied to P1-1, the output at P1-3 shall be f5. O *1. O Vdc. With P1-1 connected to P1-7, the output at PI -3 shall be to. 2 *O. 2 V. and P1-2 connected to P1-7, the output at P1-3 shall be +O.
16、2 +O. 2 V. With P1-1 disconnected from P1-7 and 3. 3. 1. 3 Test range. applied to P1-23 and P1-24, the output at P1-6 shall. be as shown in figure 2. With the type-B signals shown in figure 2 (This signal may be recurring. ) 3. 3. 1. 4 A-trigger signal. With the type-A signal shown in figure 3 appli
17、ed to Pl-35, the outputs at Pl-17 and Pl-16 shall be as shown in figure 3. (These signals may be recurring. ) Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-U-50747 12 ST777Ob 0330583 b MIL-M- 50747(MU) 8 August 1973 Input to - - - - - - - - - L
18、ogical one P1-23 - - - - Logical zero I- l.OfO.l ps I I tr and tf (40 ns (10 and 90 percent amplitude points) I I - - - - - Logical one I 1 7 Input to P1-24 - I I-I-,- -Logical Ler o tt- 1.0fO.2 ps - -+3.5*1.0 v - - - - - - - - -+0.2 f0.2 v I - Output from -d Pl -6 C 51lns Figure 2. Test Range Input
19、/Output Signal- Waveforms - - - - - - Logical one I Input to Pl-35 -1 u-,- - - Logical zero f- 1.0.*0.1 ps tr and t 40 ns (10 and 90 percent amplitude points) f- 4 i-3. 5 fl. 5 V - - - - - -to.4 *o. 4 v - - -*- I Output from I- 1.0 fO.2 ps t3.5 rtl. 5 v +o. 4 *o. 4 v - $ P1-17 Output from P1-16 4 15
20、0 t!s Figure 3, A-trigge r Input/Output Signal Waveforms 6 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,- - MIL-M-SOW LE! m vvmb OSAS- T = MIL-M- 5074
21、7(MU) 8 August 1973 -4 - - - - L - - ,Logical one - - - -. - ,Logicai one - - - - - - - - - ,Logical Aero Pulse widths = 1. O fO. 2 ps Figure 5. MALF 3 Input Signal Waveforms 3. 3. 2 Environmental 3. 3.2. 1 Storage temperature. The assembly shall meet the requirements of 3. 3.1 at ambient temperatur
22、e after exposure to and thermal stabilization at -80“ F and t160OF. 3. 3.2.2 Operating temperatures. The assembly shall meet the requirements of 3. 3. 1 while exposed to and thermally stabilized at -40F and t125OF, subsequent to which the requirements of 3.3.1 shall be met at ambient temperature. 3.
23、 3.2. 3 Vibration. The assembly shall show no physical failure and shall meet the requirements of 3. 3. 1 after being exposed to the following vibratory conditions: a. Amplitude: 1 /64 inch, constant (1 / 32 inch double amplitude) b. Vibratory motion: Simple harmonic c. Sweep time: 5 to 55 to 5 Hert
24、z in a five- minute period d. Vibration cycling: Three linear or logarithmic sweeps applied to each of the three mutually perpendicular axe s. 8 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-M-50747(MU) 8 August 1973 4. QUALITY ASSURANCE PROVIS
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