REG NASA-LLIS-0678--2000 Lessons Learned Design Considerations for Selection of Thick-Film Microelectronic Circuits.pdf

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1、Best Practices Entry: Best Practice Info:a71 Committee Approval Date: 2000-03-09a71 Center Point of Contact: JSCa71 Submitted by: Wil HarkinsSubject: Design Considerations for Selection of Thick-Film Microelectronic Circuits Practice: This guideline provides information and guidance for the design o

2、f thick-film hybrid circuits.Programs that Certify Usage: N/ACenter to Contact for Information: JSCImplementation Method: This Lesson Learned is based on Reliability Guideline Number GD-ED-2202 from NASA Technical Memorandum 4322A, NASA Reliability Preferred Practices for Design and Test.Benefit:Thi

3、s guideline identifies design considerations and reliability requirements to assure reliable performance and to avoid cost overruns due to redesign and operational failures.Implementation Method:1. Component information. The design of thick-film microelectronic circuits requires information on speci

4、fying components with established reliability. The components used in thick-film microelectronic circuits are somewhat different from the sealed or encapsulated, Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-fully tested discrete components used to

5、 fabricate circuits on printed wiring boards. The components fall into the categories of (a) thick-film resistors, (b) thin-film resistors, (c) ceramic capacitors, (d) semiconductors, and (e) thick-film conductors.2. 3. Circuit partitioning. Several factors should be considered when partitioning the

6、 system into individual microelectronic circuits. Each of the circuits should be a separate and complete function which can be tested with the addition of a minimum number of external components, and should have the minimum number of input-output pins. If a system consists of two signal paths which

7、must track, the partitioning should be done such that the corresponding circuits of each channel are in one thick-film microelectronic circuit. This will ensure that the circuit elements of both channels will be at the same temperature and therefore increase the tracking accuracy.4. 5. Packages avai

8、lable. There are several package types that are currently available in industry. The packages that are used for space flight application shall meet MIL-H-38534 requirements.6. 7. Power dissipation. The junction temperature is a function of the case temperature and the power dissipation within the pa

9、ckage. The case temperature is a function of the internal power dissipation of the microelectronic circuit, the printed wiring board loading, the thermal impedances from the package case to the outside world, and the operating ambient temperature of the chassis. Thermal impedance of packages, substr

10、ates, and semiconductors all affect the thermal gradient from the junction to the outside world. Therefore, the choice of package and the distribution of power within the package will affect the maximum allowable power of the circuit with either a fixed maximum case or ambient temperature.8. 9. Wors

11、t case analysis. A worst case analysis ensures that the circuit will function over the maximum operating temperature with the worst possible combination of component variables. The worst case analysis shall be performed in accordance with the applicable program requirements. The worst case analyses

12、shall include the individual components. Before an actual worst case analysis is started, the following preliminary considerations must be made: a. Physical limitations. There are three factors to consider: (1) the number of required pin-outs must be available in the desired type of package and a ke

13、y pin should be included in the pin count; (2) the number of components in the circuit shall not exceed the number of components specified as the maximum number that can go into that particular type of package, and (3) the use of non-established reliability components in the circuit design should be

14、 avoided.b. c. Power dissipation within the circuit. The worst case power dissipation within the circuit must be calculated.d. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-e. External factors. External factors affecting circuit performance must be

15、 identified before starting the worst case analysis; e.g., (1) the power supply tolerance should be known, (2) the worst case loading of the circuits outputs must be considered, and (3) the decoupling requirements must be considered.10. 11. Testing. Most hybrid microelectronic devices are custom mad

16、e for their particular applications. However, the part operation should be precisely defined by electrical characteristics which include all necessary parameters with test conditions, parameter minima and maxima, and parameter typical values. All active and passive elements of the hybrid should have

17、 electrical characteristics derated according to the appropriate derating factors listed in MIL-STD-975 for NASA standard parts. Derating will increase the safety margin between the operating stress level and the actual failure level for the constituent hybrid parts and will provide added protection

18、 for system anomalies unforeseen by the application engineer.12. 13. Dynamic trimming. The thick-film microelectronic circuits are dynamically trimmed using automatic laser trim system. Power supply settings, input conditions, and output requirements must be defined prior to dynamic trimming. All re

19、sistors involved in a trim must be referenced, along with the output reaction to the trimming of each resistor.14. 15. Radiation Hardness Testing. The components used in the thick-film hybrids are required to undergo radiation hardness testing when radiation tolerances are specified in the detail sp

20、ecification, which may include dose rate and latchup, total dose, and neutron irradiation as applicable.16. 17. Circuit quality level. The hybrid microelectronic circuits shall be screened to meet the requirements of MIL-STD-883, Class S or B depending on the program requirements. As a minimum, the

21、following screening steps are essential in accordance with MIL-STD-883 applicable test methods, to ensure the quality and reliability. They are, (a) Die Visual Inspection, (b) Substrate Visual Inspection, (c) Element Evaluation, (d) Package Evaluation, and (e) Quality Conformance Evaluation includin

22、g groups A, B, C, D, and E testings of MIL-STD-883 specifications.Technical Rationale:This document and JSC contractor paper, JSC 25471, provide the information and guidance to circuit designers for specifying devices which will be developed and produced as thick-film hybrid circuits. Provided by IH

23、SNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-In order to ensure a reliable circuit at the lowest cost, there are several areas that require special consideration when designing a thick-film hybrid circuit. Use of these two documents should allow the engineer to

24、 spend less time researching standards and more time designing reliable microcircuits.References:1. JSC 25471, Electrical Design Considerations for Thick-film Microcircuits2. MIL-M-38510 Microcircuits, General Specifications for3. MIL-H-38534 Hybrid Microcircuits, General Specifications for4. MIL-ST

25、D-975 NASA Standards Parts List5. MIL-HDBK-978 NASA Parts Applications Hand Book6. MIL-STD-1772 Certification Requirements for Hybrid Microcircuit Facilities and Lines7. MIL-STD-883 Test Methods and Procedures for MicroelectronicsImpact of Non-Practice: Inadequate design and selecting non-establishe

26、d reliability components may impair the reliability of hybrid microcircuits.Related Practices: N/AAdditional Info: Approval Info: a71 Approval Date: 2000-03-09a71 Approval Name: Eric Raynora71 Approval Organization: QSa71 Approval Phone Number: 202-358-4738Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-