Microsemi Update for SPWG 2017

Transcription

1 Power Matters. TM Microsemi Update for SPWG 2017 Chris Hart, Director of Marketing, Aerospace Products, Discrete Products Group Ken O Neill, Director of Marketing, Space and Aviation, Integrated Circuits and Systems Group 1

2 Overview Space products and capabilities Power hybrids and discretes RTG4 FPGA qualification update Mixed signal integrated circuits Oscillators and clocking Power Matters. TM 2

3 Microsemi Space Heritage 60 years of space flight heritage on hundreds of space programs Wide space portfolio consisting of industry-leading radiation hardened FPGAs, oscillators, atomic clocks, mixed signal IC s, discretes, and power solutions (hybrid and SMT) Complete space discrete portfolio with products on over 75% of the Defense Logistics Agency (DLA) slash sheets 40+ years of space power systems design expertise on SMT custom power supplies with zero in flight failures Internal packaging and radiation hardened by design expertise Comprehensive High Reliability Plastic/Non-hermetic Product Portfolio for low-cost "New Space" constellations Superior manufacturing and quality system ideal for high reliability applications AS9100 / ISO9001, MIL-PRF-38534, MIL-PRF-38535, MIL-PRF-19500, LEAN Continue to be a market leader in radiation hardened applications through technological innovation Leverage our breadth of technology and core strengths (packaging, radiation effects and design, quality, and reliability) Intense focus on system solutions to meet our customers needs today and tomorrow Power Matters. TM 3

4 Microsemi Space Product Overview Microsemi s Radiation Hardened Technology is found in every Satellite Sub-System Bus / Platform Payload Radiation Tolerant FPGA s High Performance and Density, Low Power TID up to 300 Krad, SEL Immune RTG4 FPGAs up to 300MHz and 150K LE RTProASIC3, RTAX & RTSX-SU QML Qualified Solar Array Electronic Power System Main Power Bus Payload Power Conditioning Radiation Hardened Power Solutions Isolated DC-DC converter modules Custom Power Supplies 2W to > 5KW Linear & POL Hybrids Rad-hard JANS Diodes, Bi-Polar Small Signal Transistors, MOSFETs, EM Relays Receive Antenna Transmit Antenna Telemetry Tracking & Control Command & Data Handling Attitude & Orbit Control Payload Interface Unit Star / Sun Sensors Magnetometer Torque Rods RF Repeater ( Bent Pipe ) Digital Communications Payload Remote Sensing Payload Space Qualified Oscillators Radiation Hardened Mixed Signal IC s Ovenized Quartz Oscillators Hybrid Voltage Controlled & Temperature Compensated Crystal Oscillators Cesium Clocks Space System Managers for Telemetry & Motor/Position Control High Side Drivers Regulators & PWMs Extensive Custom IC capability Power Matters. TM 4

5 Space Capabilities Overview Power Matters. TM 5

6 Quality and Screening Flows MIL-PRF (Radiation Hardness Assured (RHA) supported on many bipolar transistors) JAN (Joint Army Navy) MIL-PRF Performance JANTX (Extra Testing) requirements for discretes JANTXV (Extra Testing + Visual) JANS (Full Space Screening) MIL-STD-750 Test Methods 8 radiation hardness assurance (RHA) levels (M, D, P, L, R, F, G, and H) JANHC - TX Level LAT / testing for Die Sales (Bare die) Slash Sheet Specifications JANKC - Space Level (JANS) LAT / testing for Die Sales for individual device (ex. MIL- PRF-19500/123) Others - M, MA, MX, MXL (Non JAN Equivalent screening) MIL-PRF (Radiation Hardness Assured (RHA) on several hybrids) QML Classes H and K MIL-PRF QML Classes Q and V Power Matters. TM 6

7 In House Testing Capabilities to Support the Mission Total Ionizing Dose (TID) First company to supply TID rated Rad Hard BJT s to MIL-PRF slash sheets (JANSR) Working with DLA on adding ELDRS to MIL-PRF and MIL-STD-750 Testing performed per MIL- STD- 883, Method 1019 Failure Analysis Lab Scanning Electron Microscope (SEM) High magnification optical microscopes Real-time X-Ray Digital curve-tracer Micro-sectioning capabilities Chemical and mechanical decap capabilities DLA Certified Test Facility at Microsemi Lawrence, MA Cobalt-60 LDR TID gamma source JL Shepherd 484 irradiator with a Dual-Hemisphere 10 and 100 mrad (Si)/sec simultaneously Power Matters. TM 7

8 Total Ionizing Dose Expertise Fix Potential Mission Issues JANS2N2907AUB LDR Sensitivity JANS2N2907AUB Surface mount package JANSR2N2907A TO-18 through hole package Initial testing ELDRS testing on die from the same wafer lot Unbiased for this PNP transistor is worst-case (biased for HDR and unbiased for LDR) - Pass Further Investigation RGA analysis found traces of H2 in the surface mount package (lid seal) PASS FAIL Root Cause ELDRs testing with surface mount package - Fail H2 during package assembly process causes Hfe shift during LDR testing Microsemi fixed the issue through die change and elimination of H2 JANS2N2907A (Biased HDR, Unbiased LDR) Packaging can affect LDR performance JANS2N2907A - Biased JANS2N2907AUB Un biased Power Matters. TM 8

9 Space Power Products Power Matters. TM 9

10 Satellite Power System Microsemi provides customers solutions throughout all electrical sub-systems on a satellite Attitude Determination and Control Command and Data Handling (C&DH) Communications Power Distribution and Conditioning Telemetry Propulsion Power Matters. TM 10

11 Space Power Products Product Family Target Application/ Sub-System Key Differentiation Key Products Radiation Hardened Isolated DC-DC Converters Power Conditioning Unit Up Converter Blocks Power Distribution Unit System Power Bus DC-DC & PPU Ion Propulsion Thrusters Highest output power and efficiency Robust SMT construction Countless missions with no failures in space flight Greatest customization flexibility without added schedule risk Shortest lead-times SA50 Family Catalog or semicustom DC to DC power solutions w/ integrated EMI filtering. Base design has over 25 years of flight hours with 0 failures and thousands of hours of worst-case analysis Radiation Hardened Power Discretes: JANS Diodes, Bi-Polar Transistors, MOSFETs Radiation Hardened Hybrids: Linear & POL Power Conditioning Unit Up Converter Blocks Shunt Regulator Block Power Distribution Unit System Bus DC-DC Ion Propulsion Thrusters Broadest JANS QPL portfolio ELDRS guaranteed Bi-Polar Transistors Radiation Hardened MOSFETs V available DLA MIL-PRF certified facility High level of integration for footprint optimization Optimized for distrusted power architectures Largest Glass Diode and Transistor Family in the market MHP8565A (Smallest Radiation Hardened QML certified 4Amp solution on the market Ideal for low cost LEO orbits) High Voltage Electromechanical Relays System batteries Power Conditioning Unit Latching relays HV for Thrusters Vacuum sealed ultra low leakage rates Broad range of High Voltage 4KV- 10KV Highest reliability Extensive heritage in space Several hundred relays are used per satellite in various applications New investments being made in new high voltage Power Matters. TM 11

12 Space Power Hybrids Power Matters. TM 12

13 Hybrid Capabilities (Catalog and Custom Design) Supporting Aerospace and Defense Markets Quality Certification MIL-PRF Class H and K Certified Design capabilities Electrical Design (Worst-Case Analysis) Substrate Design and Fab (Thick Film) Mechanical and Thermal Design Power Module capability Custom Design or Build to print Total parts management Hybrid assembly and die attach Au and Al gold wire bonding High temperature assembly Hermetic and non-hermetic package assembly Internal electrical and radiation test Vibration or shock testing available Example Custom Products Custom Analog & Digital Interface devices D/A and A/D Converter Modules Op- Amp Modules Gated Generator Hybrid Power Supplies and Drivers BCD Decade Counters Differential Amplifiers Resistor Ladders Analog Switch modules Wide-band amplifier modules Power Matters. TM 13

14 MHP85xx Family Radiation Hardened Point of Load Hybrids Optimized for LEO Family Features Current mode control Enable Input pin for power sequencing Designed for -55C to 125C operation Peak efficiencies over 87% Worst-case accuracy less than 5% Simple external soft start circuit Nominal 500KHz switching frequency (583kHz for MHP8566) TID >100 krad (Si) for HDR and LDR SEL, SEB, SEGR, and SEFI Immune up to 85.5MeV SEU (SET) evaluated at 85.5MeV SEU (SET) immune in LEO orbit (up to 58MeV) Device Specific Features Benefits Built in DLA certified MIL-PRF Facilities (class H and K) Radiation Hardness Assurance (RHA) approved through DLA Several Vin and output current options available based on similar design to minimize component changes Optimal solution size through integrated hermetic hybrid design TID testing follows MIL-STD-883, Method High input Vin allows for operation with sufficient de-rating margin High efficiency synchronous point of load in small packaging SMD already approved on base MHP8565 design Point of Load Solution MHP8564 (SMD In Process) Vin = +4.5V to +12V (Input cap rated for +25V) Iout = 4 Amps (Parallelable to double output current and reduce ripple) Vout = to +4.5V via external set resistor or fixed out External sync pin and remote voltage sense option Ultra small 16 pin flat pack package MHP8565A (5962R13236) Vin = +4.5V to +12V (Input Cap rated for +16V) Iout = 3 Amps Vout = to +4.5V via external set resistor Ultra small 5 pin MO-078 package +120V SA50 (50W) +5V MHP8565A Dual Mode MHP8565A MHP8564 Parallel Mode Smallest radiation tolerant point of load solution on the market RTG4 FPGA VPP/VDDPLL/VD DI (3.3V) VDDI/APLL (2.5V) VDD (1.2V) Power Matters. TM 14

15 Space Discrete Unique Packages Power Matters. TM 15

16 Flex diode designed for Solar Panel Applications Qualified Used on the international space station (ISS) and other large communication satellites Optimal mounting Ultra thin construction (.5 mm), flexible, wieldable (excellent heat sync), custom lead lengths and material sets Extreme qualification Temp Cycles (5K cycles liquid to liquid -197 to 150C, 20K cycles air to air -100 to 61C) Electron (1MeV electrons with 6x10^14 el/cm^2 total fluence) Proton (45MeV protons with 6x10^6 protons/cm^2 total fluence) 20K power cycles Lead pull at multiple angles Accelerated life testing with FIT rates Weldable after moisture testing >250Mrad TID Power Matters. TM 16

17 ThinKey - Maximize power supply performance JANTXV1N & , (MIL-PRF-19500/ ) (25-150A, V, Schottky) Double plug construction, no wire bonds Surface mount with top strap available on anode or cathode Double-side cooling to maximize heat dissipation High surge capability, no internal strap or wire bonds Low inductance due to no internal strap or wire bonds Weight: grams (9x lighter than TO-254) Low thermal resistance: typical C/W No soft solder used in construction Eliminates solder creep and re-crystallization during power cycling and high temp. storage Prevents solder seal from mixing with mounting solders to ensure no compromise of the hermetic seal Pre-cap inspection easily performed prior to seal (JANTXV & JANS equiv.) Rugged ceramic and metal construction, no glass seals All die (Schottky, TVS, and rectifier) made on MSC QPL line. Power Matters. TM 17

18 Discrete and Hybrid Manufacturing Flow Wafer fab & die evaluation Die inventory Assembly & sample test Subassembly inventory Initial Test & Screen Conformance inspection Finished Goods Inventory Die inventory Assembly & sample test Subassembly inventory Initial Test & Screen Conformance inspection Finished Goods Inventory Microsemi Lawrence (160 sq ft facility) Wafer fab, JANS and SCD assembly/screening (Export controlled handling capabilities for assembly, test, screening on custom products), Package Development Microsemi Ireland (90 sq ft facility) Screening, test, verification of JANTX and JANTXV (over 600K test sockets and over 100 test methods qualified to MIL-STD-750) No major audit findings by DLA, Aviation Center of Excellence Microsemi Philippines: Assembly of non hermetic M flow devices Power Matters. TM 18

19 RTG4 FPGA Qualification Update Power Matters. TM 19

20 RTG4 Qualification and Availability MIL-STD-883 Class B Qualification Completed Successfully Product retention: 20 years at Tj 100C, or 10 years at Tj 125C ESD: Class 1A (VDDAIO passed 250V, other pins passed 2000V) MIL-STD-883 Class B flight models available today QML Class Q qualification Completion target in mid 2017 Technology insertion plan has been approved Audits completed at Microsemi, fab, bump, assembly and column vendors Standard Microcircuit Drawing (SMD) draft in progress QML Class V qualification Completion target in early 2018 Qualification uses RT4G150 in 1657-pin LGA / CCGA package 45 units from 1 wafer lot 4,000 hour life test to be completed by end of 2017 Qualification data will be submitted to DLA after life test completion EV-flow flight units to be available prior to life test completion Power Matters. TM 20

21 Programs Baselining RTG4 TESS (NASA) Orion (NASA) WFIRST (NASA) SBC (LANL) AIDA (ESA, DLR, NASA) SLIM (JAXA) Digital Channelizer (Commercial) Reconfigurable Processor (Commercial) Power Matters. TM 21

22 Introducing New CQ352 Package Resources RT4G150 Logic Elements (TMR Register + 4-Input C Logic) 151, ,824 18x18 Multiply-Accumulate Blocks RAM Mbits (1.5 Kbit and 24 Kbit Blocks, with ECC) UPROM Kbits DDR2/3 SDRAM Controller (with ECC) 2 x 32 0 PCI Express Endpoints 2 1 Globals PLLs (Rad Tolerant) 8 8 SpaceWire Clock & Data Recovery Circuits 16 4 User IO (excluding SERDES) SERDES lanes (3.125 Gbit/sec) 24 4 Hermetic, Ceramic Packages CG1657 (Ceramic Column Grid Array, Six Sigma Columns) LG1657 (Ceramic Land Grid Array, No Solder Termination) CB1657 (Ceramic Ball Grid Array, For Prototyping Only) CQ352 (Ceramic Quad Flat Pack) Available Now Samples in July Flight Units in Oct Power Matters. TM 22

23 RTG4 Radiation Summary Total Ionizing Dose Stays within parametric limits > 125 Krad (Si) Single Event Latch-Up No failure at facility limit of 103 MeV-cm 2 /mg, 100 C Configuration Upset No failure at facility limit of 103 MeV-cm 2 /mg, 100 C Flip-Flop Single Event Upset LSRAM Single Event Upset usram Single Event Upset 2.6E-12 errors/bit-day, GEO solar minimum, 1MHz 2.0E-7 errors/bit-day, GEO solar min (no EDAC) 3.1E-8 errors/bit-day, GEO solar min (no EDAC) Test plan 2017 SET: Fabric, DSP Mathblocks, clocks, SpaceWire, MSIO, MSIOD SEFI: PLL, SERDES, PCIe, DDR controllers, System Controller In-flight reprogramming Prompt dose Independent testing in progress (Aerospace, NASA, JPL, ESA) Conference Papers and Publications: SEE Symposium and MAPLD Power Point presented in 5/2016 by Melanie Berg, NASA GSFC 2016 HEART RTG4 Radiation Update A Novel 65 nm Radiation Tolerant Flash Configuration Cell Used in RTG4 Field Programmable Gate Array TID and SEE characterization of Microsemi s 4th generation radiation tolerant RTG4 flash-based FPGA 1.1E-11 errors/bit-day, GEO solar min (with EDAC) 2.7E-13 errors/bit-day, GEO solar min (with EDAC) Power Matters. TM 23

24 Mixed Signal Integrated Circuits and Space Qualified Oscillators Power Matters. TM 24

25 Radiation Tolerant Mixed Signal ICs Space System Managers LX7720 Motor Controller with Position Sensing Half-bridge drivers with current and resolver sensors for control of PMSM, BLDC, and stepper motors Samples available today Development board available today (works with RTG4 dev kit) Qualification in progress LX7730 Telemetry Manager Highly integrated acquisition of up to 64 channels, size weight power and cost saving Samples available today Development board available today (works with RTG4 dev kit) QML class V 4,000 hr life test complete, submitting qual data to DLA Released to production Full custom Mixed-Signal Integrated Circuits Radiation-tolerant, Mil-Prf screened, mixed signal ASICs 100Krad TID, SEL and SEU immunity Flight heritage on multiple programs Custom multi-device packaging Power Matters. TM 25

26 Space Qualified Oscillators Microsemi designs and manufactures Space VCXOs, TCXOs and OCXOs Precise time and frequency solutions for customers with the most demanding performance requirements 9600/9700/9800 models offer an unsurpassed combination of small size, low power and performance, 4MHz 125MHz 9500 Series Master Oscillators provide the worlds best performance for Frequency Stability and Phase Noise, up to 100MHz Heritage Programs GPS IIF, GPS III, MUOS, SBIRS, PAN COSMO IV, CLOUDSAT, Messenger, DSAC Power Matters. TM 26

27 Your Partner for Space Technology Leadership in space Leveraging our product breadth Innovative new products Focused on system solutions Power Matters. TM 27

28 Key Contacts Chris Hart Director of Marketing, Aerospace Products Discretes Power Converters Hybrids Ken O Neill Director of Marketing, Space and Aviation ken.oneill@microsemi.com RT FPGAs Mixed Signal IC s Space Oscillators Power Matters. TM 28

29 Thank You Microsemi Corporate Headquarters One Enterprise, Aliso Viejo, CA USA Within the USA: +1 (800) Outside the USA: +1 (949) Sales: +1 (949) Fax: +1 (949) Microsemi Corporation. All rights reserved. Microsemi and the Microsemi logo are registered trademarks of Microsemi Corporation. All other trademarks and service marks are the property of their respective owners. Microsemi Corporation (Nasdaq: MSCC) offers a comprehensive portfolio of semiconductor and system solutions for aerospace & defense, communications, data center and industrial markets. Products include high-performance and radiation-hardened analog mixed-signal integrated circuits, FPGAs, SoCs and ASICs; power management products; timing and synchronization devices and precise time solutions, setting the world's standard for time; voice processing devices; RF solutions; discrete components; enterprise storage and communication solutions, security technologies and scalable anti-tamper products; Ethernet solutions; Power-over-Ethernet ICs and midspans; as well as custom design capabilities and services. Microsemi is headquartered in Aliso Viejo, Calif., and has approximately 4,800 employees globally. Learn more at Microsemi makes no warranty, representation, or guarantee regarding the information contained herein or the suitability of its products and services for any particular purpose, nor does Microsemi assume any liability whatsoever arising out of the application or use of any product or circuit. The products sold hereunder and any other products sold by Microsemi have been subject to limited testing and should not be used in conjunction with mission-critical equipment or applications. Any performance specifications are believed to be reliable but are not verified, and Buyer must conduct and complete all performance and other testing of the products, alone and together with, or installed in, any end-products. Buyer shall not rely on any data and performance specifications or parameters provided by Microsemi. It is the Buyer s responsibility to independently determine suitability of any products and to test and verify the same. The information provided by Microsemi hereunder is provided as is, where is and with all faults, and the entire risk associated with such information is entirely with the Buyer. Microsemi does not grant, explicitly or implicitly, to any party any patent rights, licenses, or any other IP rights, whether with regard to such information itself or anything described by such information. Information provided in this document is proprietary to Microsemi, and Microsemi reserves the right to make any changes to the information in this document or to any products and services at any time without notice. Power Matters. TM 29