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Components for Hi-Rel Distributed Systems

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Components for Hi-Rel Distributed Systems SPACE IC GmbH Garbsener Landstraße 10 30419 Hannover Germany www.space-ic.com Tel.: +49 511 99 99 33 0 Fax: +49 511 99 99 33 10 [email protected] Managing Directors: Volodymyr Burkhay Uwe Gieselmann Marko Reuter André Rocke Register: Hannover Amtsgericht Hannover HRB 210911 High-reliability integrated circuits
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Components for Hi-RelDistributed Systems

SPACE IC GmbHGarbsener Landstraße 1030419 Hannover ▪ Germanywww.space-ic.com

Tel.: +49 511 99 99 33 0Fax: +49 511 99 99 33 [email protected]

Managing Directors:Volodymyr Burkhay ▪ Uwe Gieselmann ▪ Marko Reuter ▪ André RockeRegister: Hannover ▪ Amtsgericht Hannover ▪ HRB 210911

High- re l iab i l i t y in tegra ted c i rcu i ts

2June 2017 | © SPACE IC GmbH

Headquarter:

SICAN Technology Parkin the Northwest ofHannover, Germany

Founder Team & Management Board:

Company

• Foundation of SPACE IC in 2014 by experts from the TELEFUNKEN IC product development

• SPACE IC exclusively takes over development and manufacturing of rad-hard IC productsfrom TELEFUNKEN

A. Rocke

U. GieselmannV. Burkhay

M. Reuter

3June 2017 | © SPACE IC GmbH

Company Experience

SICANMixed-signal ASIC Design Service

1990

sciworx (Infineon)Mixed-signal ASIC Design

2000

Silicon Image Mixed-signal IP and IC Design

2007

Telefunken SemiconductorsMixed-signal IC Product Development

2009

SPACE ICMixed-signal IC Products for Space

2014Automotive Space

Industrial Medical

BCD / BCD-SOI HV-BCD (750V)

HVCMOS CMOS 2u…40n

Hirel Applications:

Technologies:

CAN Transceiver Physical IPs for Automotive since 20 Years!

4June 2017 | © SPACE IC GmbH

Overview

SPACE IC

Technical and Application Focus

• Space-Grade Analog and Mixed-Signal Integrated Circuits for Power Management and Robust Data Interfaces

IC Product Development Manufacturing:

• Chip Foundry• Wafer Test• Dicing• Assembly• Screening• Qualification Testing

Service:

• Mixed-Signal ASIC Service

• Manufacturing ServiceChip Development:

• IC Design• Package

Testing:

• Screening• Evaluation• Qualification

Chip Development:

• IC Spec• IC Design• Package Design• Prototyping

5June 2017 | © SPACE IC GmbH

Technical Focus

DC power conversion, conditioning and protection (high-voltage capability etc.):

• DC/DC Regulators

• LU Protection

• HV Gate Driver

Power Management

Robust data interfaces (high-voltage capability, high common-mode capability etc.):

• Extended Common-Mode LVDS (for SpaceWire)

• CAN Bus Line I/O

• CAN System IC

Interfaces

SPACE IC develops, manufactures and sells:

High-reliability radiation-hard analog and mixed-signal integrated circuitsfor space applications (ITAR/EAR-free)

2A point-of-load DC/DC converter fast box-to-box communication

GND shift

6June 2017 | © SPACE IC GmbH

Product Roadmap

• POL switching regulator (power distribution) SPPL12420RH• LVDS Rx extended CM receiver (data communication) SPLVDS032RH• LVDS Tx transmitter (data communication) SPLVDS031RH• HV-POL next generation POL product SPPL14065RH

2015 2016 2017 2018

HV-POL (EM)LVDS

POL (ESCC)POL (EM) POL (FM)

7June 2017 | © SPACE IC GmbH

Power Distributionwith POL

• Modular approach with improved re-use possibilities using intermediate power busses and standard power interfaces

• Highly efficient and accurate power conversion at point-of-load

• Weight & volume of few power rails; lower current

8June 2017 | © SPACE IC GmbH

SPPL12420RH

• Ceramic hermetic flatpack package

• SOI technology

• 2A continuous output load current

• 24V input voltage capability

• 4.5V min. input voltage

• 0.923V min. output voltage

• >90% efficiency

• 340kHz fixed switching frequency

• -55°C to +125°C extended temperature range

Features

80%

90%

100%

0 1 2

Effic

ienc

y

Iout [A]

VIN = 5 V

VIN = 6 V

VIN = 12 V

VIN = 18 V

VOUT = 3.3 V

9June 2017 | © SPACE IC GmbH

TID Wafer Lot AcceptanceSPPL12420RH

ESCC 22900

TID test campaign at ESTEC 60Co Radiation Facility

Setup:

• 12 DUTs under worst case biasing andload conditions(VIN = 12 V, ILOAD = 0.4 A)

• 3 DUTs unbiased

• Dose rate = 360 rad/h

• 6 extra DUTs as reference group

• Comprehensive testing of datasheet parameters at irradiation stops

Results:

• Biased parts passed 40 krad(Si)

• Unbiased parts passed 105 krad(Si)

3,0

3,1

3,2

3,3

3,4

3,5

3,6

0 5 10 15 20 25 30 35 40krad(Si)

IRRADIATION

0 24h

RTA

0 24 48 72 96 120 144 168h

HT AGEING

VOU

T [V

]

10June 2017 | © SPACE IC GmbH

ESCC 25100

Heavy Ions TestSPPL12420RH

SEE test campaign at RADEF Accelerator Laboratory

Conditions:

• 8 application boards configured for VOUT = 1.2/1.8/2.5/3.3/5.0/12V (3 boards with sockets)

• Worst case configuration for destructive events (most sensitive tilting)

Results:

• Max. safe VIN for destructive event free operation in any configuration:

– VIN = 11V for effective LET of ~89 [MeV∙cm2/mg]– VIN = 13V for effective LET of ~60 [MeV∙cm2/mg]

• No dependency of destructive SEE event sensitivity on VOUT or its relation to VIN

• Worst case transients in any configuration result in voltage drops max. 5% of VOUT with duration of a few µs

• The most transients result in voltage drops<3% of VOUT

11June 2017 | © SPACE IC GmbH

SPPL12420RH Heritage

• In-orbit verification of SPPL12420RHin cooperation with Berlin Space Technologies

• SPPL12420RH Engineering Model on special application evaluation board:

– VIN = 24V– continuous operation

• Telemetry of VIN and VOUT values

2015

Optional Enable Control

ADC (≤2.5V)

ADC (≤2.5V)

ThermalConnect

GND

VIN (≤25V)

ON: 3..6VOFF: 0V

• Singapore earthobservation satelliteto support disastermonitoring in Asia

• Launched onDecember 16th, 2015into 550km near equatorial orbit

• Telemetry data shows persistent proper operation of the SPPL12420RH

In-Orbit Demo

12June 2017 | © SPACE IC GmbH

• Compliant to TIA/EIA-644-A

• Extended Common-Mode

• 0 to 400Mbps over single wire pair

• HV robustness, Latch-Up immunity

LVDS TX & RX

• Fast point-to-point data transfer with exceptional ground noise immunity

• Suitable for SpaceWire networks

• Suitable to replace RS-422 or RS-485

AdvantagesCommunication

Module A

Tx

Module B

Rx

LVDS 400 Mbps

-7V … +12VGNDA GNDB

13June 2017 | © SPACE IC GmbH

SPLVDS031RH & SPLVDS032RH

• Very low skew

• Low current consumption

• ESD HBM >8kV

• -55°C to +125°C extended temp. range

• Ceramic hermetic FP-16 package

• SOI technology

• 400Mbps quad LVDS line translator

• -7V to +12V extended common mode

Features

SPLVDS031RH SPLVDS032RH

LVDS signal:

• 400Mbps

• PRBS23

14June 2017 | © SPACE IC GmbH

Conditions:• TID without applied bias• Dose rate: 75rad/min (60Co source)• Room temperature annealing• Hot temperature annealing 100°C for 5hResults:• Minor shifts in key data sheet parameters

after TID irradiation up to 100krad• None of the specifications are violated• All tested parts keep full functionality

-2%

0%

2%

4%

6%

8%

10%

12%

pre

radi

atio

n

5kra

d

10kr

ad

20kr

ad

40kr

ad

100k

rad

afte

r roo

mte

mpe

ratu

rean

neal

afte

r hot

tem

pera

ture

anne

al

drift

High-impedance output current

Differential output voltage

Steady-state output cm voltage

Output short circuit current

Power supply current (disabled)

Power supply current (loaded)

Conditions:• TID without applied bias• Dose rate: 75rad/min (60Co source)• Room temperature annealing• Hot temperature annealing 100°C for 5hResults:• Minor shifts in key data sheet parameters

after TID irradiation up to 100krad• None of the specifications are violated• All tested parts keep full functionality

-1%

0%

1%

2%

3%

4%

5%

pre

radia

tion

5kra

d

10kr

ad

20kr

ad

40kr

ad

100k

rad

afte

r roo

mte

mpe

ratu

rean

neal

afte

r hot

tem

pera

ture

anne

al

drift

Output short circuit current

LVDS input termination resistor

LVDS input current @ -7 V

LVDS input current @ +12 V

Power supply current (static)

Power supply current (disabled)

SPLVDS031RH & SPLVDS032RH TID Tests

SPLVDS031RH SPLVDS032RH

15June 2017 | © SPACE IC GmbH

SPLVDS031RH & SPLVDS032RHHeavy Ions Test

Conditions:• Static test mode #0 (external fail-safe NW) • LET 65.2MeV/(mg/cm2) Results:• No fails (SEL, SEGR, SEB)• SET event - single bit error

Conditions:• Static test mode #0• LET 65.2MeV/(mg/cm2) Results:• No fails (SEL, SEGR, SEB)• SET event - small variation of output

magnitude (<100mV, 25ns)

SPLVDS031RH SPLVDS032RH

16June 2017 | © SPACE IC GmbH

Outlook

• Focus on general purpose ICs with significant quantities per satellite• Based on SPACE IC technology and development portfolio:

Power Management, e.g.

DC/DC Regulators LU Protection HV Gate Driver

Robust Interfaces, e.g.

SpaceWire LVDS CAN Bus Line I/O CAN System IC

New Developments

Share your requirements with our experts and define the next generationITAR/EAR-free space-grade product according to your needs.

[email protected]

www.space-ic.com

Thank you for

your attention!


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