Advanced, Hardened By Process Microelectronic Products For Next
Transcript of Advanced, Hardened By Process Microelectronic Products For Next
Honeywell 1Copyright 2009 Honeywell International Inc May be published with permission by JAXA 2009
Advanced, Hardened By Process
Microelectronic Products
For Next Generation Space Systems
October 15, 2009
Honeywell 2Copyright 2009 Honeywell International Inc May be published with permission by JAXA 2009
Presentation Summary
• Introduction
• S150 150nm Rad Hard Process
•SOI CMOS Technology
•Trusted Foundry and Quality
• ASIC Platform And Design Flow
• Standard Products
•Memories
•SerDes
•ADC
•Processors
• Summary
Honeywell 3Copyright 2009 Honeywell International Inc May be published with permission by JAXA 2009
Introduction
Honeywell Is An Experienced, Fully Qualified Supplier Of Space
Microelectronics
- Four Generations Of Digital ASICs For Space
- Over 700 Space ASICs Developed And Flown
- Five Generations Of SRAM Products For Space, From Legacy
256K To Leadership 64M Densities
- ASIC Design Resources Across The USA and Globally
- SOI CMOS Technology Built In Our Trusted Foundry
- QML Certified Products And Processes
- Semiconductor Industry Experienced Management Team
Honeywell 4Copyright 2009 Honeywell International Inc May be published with permission by JAXA 2009
Trusted Foundry Accreditation
Process Name
.7 um
SOI-4
.35 um
SOI-5
150nm
S150
Unclassified
Wafer FabAccredited Accredited Accredited
Classified
Wafer FabAccredited Accredited Accredited
ASIC Design Classified Or Unclassified
Classified Or Unclassified
Classified Or Unclassified
ASIC Design Flow
Several Synopsys Synopsys
ASIC Assembly
Classified Or
Unclassified
Classified Or
Unclassified
Classified Or
Unclassified
ASIC TestClassified Or
Unclassified
Classified Or
Unclassified
Classified Or
Unclassified
Mask Making
In USA In USA In USA
Process
Flows
Digital RH
Mixed Sig. RH
Mixed Sig. RF
High Temp
Digital RH
Mixed Sig. RH
Mixed Sig. RF
High Temp
4LM Rad Hard
6LM Rad Hard
8LM Rad Hard
6LM NV SRAM
Aerial View Of Honeywell Trusted Foundry Campus
Honeywell 5Copyright 2009 Honeywell International Inc May be published with permission by JAXA 2009
SOI CMOS Wafer Processes
Buried SiO2 Layer Provides- Radiation Hardness
- Ultra High Reliability
- Faster Circuits At Same Process Node
- Lower Power At Same ProcessNode
- Excellent Isolation For Mixed Signal ASICs
- Continuous High Temp Operation At 225°C
SOI CMOS
Bulk CMOS
N+ P+ P+
S DG S DG
Silicon Substrate
N+
Silicon Substrate
SiO2
High Capacitance Region Substantially Reduced By Buried Oxide Layer
Bulk CMOS
N+ N+ P+ P+
S DG S DG
SiO2
Silicon Substrate
N+N+
Silicon Substrate
Transistor Cross SectionsProcess Name
SOI-4 SOI-5 S150
Production*Now Thru
2015+Now Thru
2015+Now Thru
2015+
Interconnect4 Level CuAl
4 Level CuAl
4-8 Level CuAl
Gate Length .7 um .35 um 150 nm
Wafer Size 150 mm 150 mm 200 mm
DevicesNCh, PCh,
DMOSNCh, PCh,
DMOSNCh, PCh, MIMCAP
Vdd (V) 3.3-20 3.3 3.3/2.5/1.8
Hardened By
Process Process Process
Process
Flows
Digital RH
Mixed Sig. RH
Mixed Sig. RF
High Temp
Digital RH
Mixed Sig. RH
Mixed Sig. RF
High Temp
4LM Rad Hard
6LM Rad Hard
8LM Rad Hard
6LM NV SRAM
* Assured Source Of Supply To Major Programs For United States Government
Honeywell 6Copyright 2009 Honeywell International Inc May be published with permission by JAXA 2009
Why SOI (Silicon on Insulator)?
• High-Temperature Operation
• Low Leakage, High Isolation resistance & Low Parasitics
• Low Power Operation
• Radiation Hard Operation- Greatly reduced sensitive
volume
- Reduced error rate for unhardened circuits
- Reduced overhead for hardening
- Latch-up immune
• Electro-Optic capability
SOI
Bulk
SOI
Honeywell 7Copyright 2009 Honeywell International Inc May be published with permission by JAXA 2009
Radiation Hardened By Process
• SOI And Radiation Hardness
- Rad Hard By Process – SOI CMOS Wafer Technology Is “Hard”
- Circuit Design And Layout Techniques Implemented To Further Improve Radiation Hardness Total Dose: > 1 X 106 Rad(Si)
Soft Error Rate: 1 X 10-11 Upsets/Bit-day
Transient Dose Rate
• Upset: > 1 X 1011 rad(Si)/S
• Survivability: > 1 X 1012 Rad(Si)/S
Neutron Fluence: 1x1014 N/Cm2
No Latchup
• Performance Benefits
- Minimum Area Required To Meet Rad Requirements
- Improved Speed, Power And Density Reduced Capacitance From SOI Technology
10-30 dB Lower Cross-talk Than Bulk Silicon
Higher Density From Small Cell Design
Honeywell 8Copyright 2009 Honeywell International Inc May be published with permission by JAXA 2009
Advanced Space ASIC Platforms
PlatformHX2000
HMX2000
HX3000
HMX3000
HX5000
HMX5000
Structured Array
SOI CMOS Process
0.7 um 0.35 um 150 nm 150 nm
# Base Arrays 5 4 7 1
Max # I/O 372 472 1000 824
Useable Gates 40-390K* 235-1,200K* 2-15M* 3-5M*
Design IPHoneywell, Customer
Honeywell, Customer
Honeywell SERDES,
Synopsys**
Honeywell Synopsys**
Device TypesNch,Pch, Lincap, DMOS, Inductor,
CrSi Resistor
Nch,Pch, Lincap, DMOS, Inductor,
CrSi Resistor
Nch, Pch, MIMCap
Nch, Pch, MIMCap
Available Now Now Now 2010
* Maximum Number Depends On Mix Of Logic And Memory **From Synopsys DesignWare IP Library
Honeywell 9Copyright 2009 Honeywell International Inc May be published with permission by JAXA 2009
HX5000 ASIC Features• Up to 15M gates• Core operating speed >
500MHz• I/O Speeds 500 MHz• Full military temp (-55C°
to 125C°)• BGA & flip chip high rel
packaging• Standard Cell Library
HX5000: 150-nanometer Rad-Hard Family
Advanced Technology• 200mm (8”) wafers• 150nm gate length• 8 layer metal• Low Power (1.8V core)• I/O Compatibility (3.3/2.5/1.8V)
Rad Hard Performance• Total dose 1Mrad(Si)• SER <1E-11 e/bd• Prompt Dose 1E11 rad(Si)/s • Neutron 1E13 MeVeq n/m2
16Mb SRAM
4Mb SRAM
1Mb MRAM
Structured ASIC
SERDES4 TX
Lanes
4 RX
Lanes
PLL
Block
4 TX
Lanes
4 RX
Lanes
SERDES8HM
SERDES8SM
4 TX
Lanes
4 RX
Lanes
4 TX
Lanes
4 RX
Lanes
8 CH
Common
SERDES8_TOP
4 TX
Lanes
4 RX
Lanes
PLL
Block
4 TX
Lanes
4 RX
Lanes
SERDES8HM
SERDES8SM
4 TX
Lanes
4 RX
Lanes
4 TX
Lanes
4 RX
Lanes
8 CH
Common
SERDES8_TOP
DRVDD DRGND D1 D0 DCO OEB AVDD AGND(5) AVDD CLK- CLK+ AGND(5)
cf 48 47 46 45 44 cf cf 43 42 41 cf cf 40 39 38 37 cf
d_crnr d_vdd d_vdd d_vss d_vss d_ d_ d_ d_vdd d_vss d_vss a_vdd a_vss a_ a_vdd a_vdd a_vss a_vss a_vss a_vdd a_vdd a_clk_ a_clk_ a_vss a_crnr
_d2 io_pc io_pc io io dout dout clkout io_pc io _d3 a_pc a_pc shmit_ a_pc a_pc a_pc _d1 a_pc a a_pc r_hvt r_hvt a_pc _d1
in_hvt
vssfl (2) vssfl
vdddr vdddr vssdr vssdr d1 d0 dco vdddr vssdr vssfl vddfl vssmd oe_b vddmd vddmd vssmd vssfl vssclk vddclk vddclk clkinn clkinp vssclk
s s s s s s
o o o o
d2 PC PC VSSIO PC o d3 o PC VSSA PC PC PC o d1 o PC PC VSSA PC d1
o | o s pwdn 36 PDWN
D2 1 d2 s VDDIO | PC VDDA VDDA a_shmit_in_hvt
d_dout | V V t ad9246 cf (4)
D3 2 d3 s o VSS | VSS o D S a_shmit_in_hvt
d_dout | D S t enc125 cf (4)
D4 3 d4 s VDD | A A a_shmit_in_hvt
d_dout o --|-- vddclk
cf vssfl o d2 pad a_vdda
d_vss_d2 PC vssclk cf
vddfl PC PC power clamp o a_vssa_pc
d_vdd_pc s pad to pkg signal land d1 o vssfl(2) cf
vdddr PC pad name t pad to pkg tie-off land o a_vss_d1
d_vddio_pc I/O name corner pad to vssfl PC vsssha cf
vssdr a_vssa_pc
d_vssio 48 pin no planes pkg wirebond land s rbias 35 RBIAS
D5 4 d5 s V V V V a_bias_r
d_dout S D S D # single wirebond to pkg pin # s cml 34 CML
D6 5 d6 s S D S D #pads a_bias_r
d_dout I I PC vddsha
D7 6 d7 s O O # double wirebond to pkg pin # a_vdda_pc 33 AVDD
d_dout PC vddsha
vssdr PC a_vdda_pc
DR 7 d_vssio_pc cf single wirebond to pkg cavity floor vsssha 32 AGND(5)
GND vssdr V V V a_vssa
d_vssio vssfl vssfl S D S s vin 31 VIN-
vdddr | I/O I/O | S D S a_vin_r
DR 8 d_vddio | | o A A s vip 30 VIN+
VDD vdddr PC o o o o d1 a_vin_r
d_vddio_pc d2 I/O PC vsssha cf
vddfl PC I/O o a_vssa_pc
d_vdd_pc o VSSIO = vssdr d1 o vssfl(2) cf
cf vssfl o d2 I/O VDDIO = vdddr Direction o a_vss_d1
d_vss_d2 vssfl -------------------------------------------------- o I/O VSS = vssfl N PC vssref 29 AGND(5)
D8 9 d8 s o o -------------------------------------------------- vssfl VDD = vddfl W + E a_vssa_pc
d_dout S vddref
D9 10 d9 s o d2 I/O I/O d1 o VSSA = vssmd & vssclk & vsssha & vssref -------------------------------------------------- a_vdda
d_dout -------------------------------------------------- VDDA = vddmd & vddclk & vddsha & vddref s reft 28 REFT
D10 11 d10 s -------------------------------------------------- a_ref_r_hvt
d_dout -------------------------------------------------- --|-- V V s refb 27 REFB
D11 12 d11 s VDD | D S a_ref_r_hvt
d_dout | D S s vref 26 VREF
vssdr PC o VSS | VSS o d1 o o A A a_vref_r
d_vssio_pc | o s sense 25 SENSE
vdddr PC VDDIO | VDDA VDDA a_vref_r
d_vddio | (6) PC vssref cf
cf vssfl o d2 o d2 o PC VSSIO PC o d3 o VSSA PC PC PC PC o d1 o PC VSSA PC o d1 o a_vssa_pc
d_crnr_d2 o o o vssfl cf
s s s s s s a_crnr_d1
d12 d13 or vssfl vssdr vssdr vdddr vdddr spi_sd vssdr vssfl spi_sc spi_ vssfl vssfl vddfl vddfl vssfl vssref vssref vssref vddref vddref
io_dcs lk_dfs csb (2) _db2
d_ d_ d_ d_vss d_vss d_vss d_vdd d_vdd d_ d_vss d_vss a_ a_ a_vss a_vss a_vdd a_vdd a_vss a_vss a_vss a_vss a_vdd a_vdd
dout dout dout _d2 io_pc io io io_pc bidir io _d3 shmit_ shmit_ a_pc a_pc a_pc a_pc _d1 a_pc a ref_d1 a a_pc
in_hvt in_hvt
13 14 15 cf 16 17 18 cf 19 20 21 cf 22 cf cf 23 cf 24
D12 D13 OR DRGND DRVDD SDIO/DCS SCLK/DFS CSB AGND(5) AVDD AGND(5) AVDD
total
25
23
23
24
95
top
bottom
left
right
#I/O
23
23
22
23
91HMXADC9246
Honeywell 10Copyright 2009 Honeywell International Inc May be published with permission by JAXA 2009
HX5000 / S150 Capability
QML Complete:
• QML Certification Received – 4/7/07
• S150H Technology QML Qualification Received –4/22/08
• 16M SRAM QML Qualification Received –4/22/08
• HX5000 QML Qualification Received – 11/18/08
HX5000/S150 Successes:
• PDV 1.6M gates
• QTV 3.9M gates
• 4M SRAM
• 16M SRAM
• 1M MRAM
• Quad SerDes Std Prod
• Customer ASIC 1 6.9M gates
• Customer ASIC 2 4.0M gates
• Customer ASIC 3 12.4M gates
Honeywell 11Copyright 2009 Honeywell International Inc May be published with permission by JAXA 2009
Structured Array Features
• S150-based (0.15µ) ASIC platform combining advantages of gate array with the flexibility of standard cell
- Same wafer technology as HX5000
- Proven memory and PLL macros
- HX5000 ASIC NRE tools and flow
- Up to 15% faster than HX5000
- Provides ASIC NRE cost and schedule advantages
• 3M to 5M usable logic gates
• Dual port SRAM - 1.9M bits
• 10 instances 512x36
• 14 instances 1024x36
• 14 instance 2048x36
• 4 Phase Locked Loops (PLLs)
• 512 signals, many I/O options
Parameter Requirement
Total Ionizing Dose > 1 MRad(Si)
Single-Event-Upset
(Adams’ 90% Worst
Case Environment)
SEU_NORMAL < 1E-8 e/b-d
SEUT1 < 1E-9 e/b-d
SEUT2 < 1E-10 e/b-d
SEUT3 < 1E-11 e/b-d
Single-Event-Latchup Immune
Neutron Irradiation >1E12 Mev eq. n/cm2
Dose-Rate Upset > 1E9 Rad(Si)/s
Dose-Rate Survivability >1E12 Rad(Si)/s
Honeywell 12Copyright 2009 Honeywell International Inc May be published with permission by JAXA 2009
QML Qualified, Synopsys Based HX5000 Design Flow
Chip
Specification
Development
Synthesis
RTL
Design
Verification
Floorplan
Physical
Synthesis
ASIC
Fabrication
Package
Requirements
Test
Requirements
Package
Development
Test
Development
Assembly
Test
Screening
Place and
Route
System
Specification
Development
DFT
QML Design Flow
Trial Place And RouteRTL Refinement
and Optimization
Typical Responsibilities
Customer Customer-Honeywell Honeywell
Working Silicon On
12.4M Gate, 64 Bit
RISC Processor
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Validated SERDES Design IP
• Supports Multiple Standards
- 10GE (4x3.125 Gb/s XAUI)
- 10G Fibre Channel (4x3.1875 Gb/s XAUI)
- 1G/2G Fiber Channel
- 1G Ethernet
• Low Power
- 185 mW Per Channel @ 1.8V
- 8 Lanes With A Single VCO
• Ready To License & Design-In Today
- DoD Approved At TRL7
- Completed All Radiation Testing, Exceeding Customer Requirements
- Hard & Soft Macro In 150nm Library Now
• High Signal Integrity
- Superior Distance
FR4 backplane > 1m @ 3.125 Gbps
Infiniband cable > 15m @ 3.125 Gbps
- Margin Increases At Lower Data Rates
- Low jitter
TX DJ = 0.20 UI, TX TJ = 0.33 UI
RX DJ = 0.33 UI, RX TJ = 0.62 UI
- BER Of <1e-14
• Individual Channel Programmability
- Selectable Data Rate
- Selectable Signal Shaping For Optimization Of Individual Channels
Validated SERDES On 150nm Rad Hard Process
Honeywell 14Copyright 2009 Honeywell International Inc May be published with permission by JAXA 2009
SERDES Standard Product
Product Features• Quad SERDES, Redundant Serial I/O
• Parallel Interface Using SSTL2 I/O
• 468 Pin LGA Package
• Evaluation Board, Data Sheet, Users
Manual And Pricing Available Now
Protocol Support• 1 To 3.1875 Gb/Sec For General Backplane
Applications
• 1G/2G/10G (XAUI ) Fibre Channel
• 1G And 10G (XAUI) Ethernet
JTAG MDC/MDIO CMU
(PLL and
Clocks)
Configuration
and Control
Registers
4 Channels Port A
4 Channels Port B
RX 2:1 MUX
4 Channels Port A
4 Channels Port B
Parallel Interface
4 Channels
4 Channels
RX 8
8
8
8
RXD_0
RXD_1
RXD_2
RXD_3
TX 8
8
8
8
TXD_0
TXD_1
TXD_2
TXD_3
Port A RX Diff Pairs TX Diff Pairs
8
8
8
8
8
8
8
8
RX0_A
RX1_A
RX2_A
RX3_A
TX0_A
TX1_A
TX2_A
TX3_A
Port B RX Diff Pairs TX Diff Pairs
8
8
8
8
8
8
8
8
RX0_B
RX1_B
RX2_B
RX3_B
TX0_B
TX1_B
TX2_B
TX3_B
Honeywell 15Copyright 2009 Honeywell International Inc May be published with permission by JAXA 2009
SERDES Evaluation Kit
• Contents- 8 Channel SERDES Board
- Cables
- Software and Documentation
• Mates To Existing Backplane For At Speed Characterization
• Multiple Programmable Configuration Interfaces
- External USB
- External MDC/MDIO
- FPGA
- On-board Jumpers
• Xilinx4 FPGA Interface To SERDES via
SSTL2 Bus - Use Application Code With SERDES
Honeywell 16Copyright 2009 Honeywell International Inc May be published with permission by JAXA 2009
Static RAM Product Family Overview
Organization Package Delivery Spec Sheet
HX6256 256K (x8) 28 DIP, FP Now www.honeywell.com/radhard
HLX6256 256K (x8) 28 DIP, FP Now www.honeywell.com/radhard
HX6228 1M (x8) 32 Or 40 FP Now www.honeywell.com/radhard
HLX6228 1M (x8) 32 Or 40 FP Now www.honeywell.com/radhard
HX6408 4M (x8) 36 FP Now www.honeywell.com/radhard
HXS6408 4M (x8) 36 FP Now www.honeywell.com/radhard
HXSR01608 16M (x8) 40 FP Now www.honeywell.com/radhard
HXSR01632 16M (x32) 86 FP Now www.honeywell.com/radhard
HXNV0100 1M (x16) 64 CQFP EM Now www.honeywell.com/radhard
HXSR06432 64M (x32) 86 FP Now www.honeywell.com/radhard
QML Qualified Memories For Space Applications
Honeywell 17Copyright 2009 Honeywell International Inc May be published with permission by JAXA 2009
Rad-Hard 16Mbit SRAM
• Designed For Radiation Sensitive Environments
• Available as 2M x 8 or 512K x 32
• SEU Hardened With No Internal EDAC Implemented
• Target Applications - Reconfigurable Space Processors
- Payload Computers
- Navigation Computers
• Key Specifications- Organization: 2M x 8 or 512K x 32
- Operation: Asynchronous
- Access Time: 13ns Typ @ 1.8V, 25oC
- Core Voltage: 1.8 Volts
- I/O Voltage: 2.5 / 3.3 Volts
- Package: 40 Pin Flatpack x8 Option86 Pin Flatpack x32 Option
- Power (50MHz, x8 option): < 270mW @ 25oCStandby Current: < 5mA @ 25oC
Honeywell 18Copyright 2009 Honeywell International Inc May be published with permission by JAXA 2009
Rad-Hard 4Mbit SRAM
• Manufactured on 150nm technology
• Form, Fit, and Function of existing HX6408
• Faster Access Times
• Lower Dynamic Power
• Key Specifications
- Organization: 512k x 8
- Operation: Asynchronous
- Access Time: <10ns typical
- Supply Voltage: 3.3 Volts
- I/O Voltage: 2.5 / 3.3 Volts
- Package: 36 Lead Flatpack
- Dynamic Current: <1mA/MHz
Honeywell 19Copyright 2009 Honeywell International Inc May be published with permission by JAXA 2009
HXSR06432 64M SRAM Memory Module
• Uses A 4-High Stack Of 512K X 32 SRAM Die
• Configured As 2M X 32
• 86 Lead Flatpack
- 1.23 X 0.96 X 0.19 In
- Vs 16M SRAM:1.13 X 0.85 X 0.16 In
- Saves 75% Of Board Space
• Engineering Model Orders Now
• Production Upgrade Q4 2009
HXSR06432 SRAM Module
Honeywell 20Copyright 2009 Honeywell International Inc May be published with permission by JAXA 2009
HXNV0100 1M Non Volatile MRAM Product
• 64K X 16-bit Non-volatile Memory- No Data Loss On Power Down Or Power
Interruption
• Radiation Hardened For Strategic Applications
• 0.15 micron Silicon-On-Insulator process
• No Wear Out - Unlimited Writes
• Non-destructive Readout (NDRO)
• Magneto-resistance (MRAM) Memory Bits
• Magnetically-shielded 64-pin Ceramic Package
• Error Correction Code (ECC)- Single EDAC Per Address
• Performance- < 70 nS Read Cycle Time
- < 100 nS Write Cycle Time
- < 500 mW Active Power
- < 100 mW Standby Power
- 1.8V Core And 3.3v I/O
Honeywell 21Copyright 2009 Honeywell International Inc May be published with permission by JAXA 2009
HMXADC9225 12-bit A/D Converter
• Radiation Hardened Monolithic 12-bit A/D Converter• 25 MSPS, 4 Stage Pipeline Architecture• On-chip Sample-and-hold Amplifier • Single +5volt Analog Supply• 5V Or 3.3V Digital Tri-state I/O• Requires External 1-2 Volts Vref • 28-lead Space Qualified Ceramic Package
• Performance- Rad Hard to >1M Rad(Si) TID- No Latchup - No Missing Codes Guaranteed- Differential Non-Linearity Error: 0.4 LSB- Straight Binary Output Data- Signal-to-Noise and Distortion Ratio: 69.6 db- Spurious-Free Dynamic Range: - 81 db- Typical Low Power: 345mW
Honeywell 22Copyright 2009 Honeywell International Inc May be published with permission by JAXA 2009
14-bit A/D Converter (HMXADC9246)
• Conversion of Commercial AD9246 To Honeywell’s Rad Hard S150 Process
• 14-bit Pipeline A/D
• Sample Rate Up To 125 MSPS
• Power Supplies- 1.8V analog supply
- 1.8 to 3.3V output supply
• Flexible analog input- 1V p-p to 2V p-p input range
In Design Now, Ready To Sample In Mid 2010
Honeywell 23Copyright 2009 Honeywell International Inc May be published with permission by JAXA 2009
RHPPC - Based on Freescale PowerPC 603e
• 32 Bit Microprocessor
• Licensed From Freescale Semiconductor
• 100% Compatible With Freescale Power PC 603e Processor
- Operating System
- Software Development Tools
- Function
• Key Specifications- Core frequency up to 80 MHz
- Programmable integrated PLL
- Power Supply = 3.3 V ± 0.3 V
- Power Dissipation: 7.6W max, 3.6V, 125°C, (GCLK=80 MHz, SYSCLK=20MHz)
- Radiation Performance
Total Ionizing Dose: >300krad(Si)
Soft Error Rate: <1.5x10-5 Upsets/processor-day
- Up to five instructions in execution per cycle.
- Single cycle throughput for most instructions
Five independent execution units and two register files
- Branch Processing Unit (BPU) for static branch prediction
- Integer Unit with 32 32-bit General Purpose Registers (GPR)
- Fully IEEE 754-compliant Floating Point Unit (FPU) with 32 32-bit Floating Point Registers (FPR),
- Load Store Unit (LSU) for data transfer between data cache and GPRs and FPRs
- System Register Unit (SRU) that executes condition register (CR), special-purpose register (SPR) instructions, and integer add/compare instructions
Honeywell 24Copyright 2009 Honeywell International Inc May be published with permission by JAXA 2009
Radiation Hard Analog and Digital SSI components
-RS422 Driver
-RS422 Receiver
-LVDS Driver
-LVDS Receiver
-Quad Nand Gate
-BUS Transceiver
-Analog Multiplexer
-Comparator
-Dual Operational Amplifier
-Digital to Analog Converter
Honeywell is currently productizing the following production SOI CMOS rad hard digital and analog SSI components:
Honeywell 25Copyright 2009 Honeywell International Inc May be published with permission by JAXA 2009
ASIC Test Capability
• Testing Capabilities High Speed Digital To 3+ Gbps
High Pincount To 1024 Pins
High Density Memory
Precision Analog
Multiple Burn-In Test Systems
• Certifications MIL-PRF-38535 (QML)
Class Q/B Tactical Devices
Class S/V Space Devices
MIL-STD-883 Screening
For Testing Classified Products
• In House Test Engineering Team
• Advanced Tester Systems
ITS9000 CX Digital – 320 I/O @ 80MHz For HX2000
ITS9000 FX Digital – 320 I/O @ 100MHz For HX3000
ITS9000 EXA8000-300 – 960 I/O @ 800 Mbps For HX5000
AEHR ATX3200, MCC HPB5 And EJ Systems For Burn-In
ITS9000 EXA8000-300 High Speed Tester For Testing Classified or
Unclassified ASICs With Up To 960 I/O At Speeds Up To 800 Mbps
Honeywell 26Copyright 2009 Honeywell International Inc May be published with permission by JAXA 2009
ASIC Assembly Capability
• Plant Large Assembly Facility
Class 1000 Clean Rooms
Class 100 Hoods For Inspection And Lid Seal
Continuous Environmental Monitoring
• Certifications QML (MIL-PRF-38535) For SCP & MCMs
Class Q/B Tactical And Class S/V Space Devices
DSCC (MIL-STD-883) Screening Test Methods
Assemble Classified Products
• In House Package Design Engineering Team ASIC Assembly Facility
Honeywell 27Copyright 2009 Honeywell International Inc May be published with permission by JAXA 2009
Summary
• Honeywell Is An Experienced, Fully Qualified Supplier Of Space
Microelectronics, Ready To Work Directly With You To Apply Our
Capabilities To Your Programs
- Four Generations Of Digital ASICs For Space
- Strategic Partnership With Synopsys Design Automation
- Over 700 Space ASICs Developed And Flown
- 12.4M Gate, 64 Bit RISC Processor Built On HX5000 In 2008
- Five Generations Of SRAM Products For Space, From Legacy
256K To Leadership 64M Densities
- ASIC Design and Verification Resources
- SOI CMOS Technology Built In Our Trusted Foundry
- QML Certified Products And Processes
- Semiconductor Industry Experienced Management Team