Launch your Vision Company Presentation

Company Presentation

SpaceTech GmbH

Launch your Vision

Developments for 30 Missions 592 Satellites 1763 Equipments

In Orbit on 10 Missions 50 Satellites 107 Equipments

And more to come…

EUCLID

NGSAR

JASON/S6

JUICE

C-SAT

OneWeb860 Satellites

MERLIN

LAPAN A4

York

IMECES5

GFO

S5-P

GK-2

K-3

OneWeb40 Satellites

FS-5

S2

Space IL

ICARUS

20202004 2009 2014

NAOS

CRISTALROSE-LCHIMECO2MLSTM

Company Profile

Business Areas Small Sat. Missions

Optical Instruments

Satellite Equipment

Facts & Figures Foundation: 2004

Staff: 90 (avg. age 39)

Yearly Turnover: 20 M€

We stand for Institutional and New Space

Smart & reliable Designs

High Cost Efficiency

Man. Directors: W. Pitz (CEO), F. Gilles, B. Doll

SpaceTech GmbHSeelbachstrasse 9-11-13

88090 Immenstaadwww.spacetech-i.com

International customers

International workforce

Company Portfolio & Heritage examples – more than 100 equipments in orbit

Systems Mission Design

Small Satellites

End-to-End systems

Instruments

Laser Instruments Structures & Mechanisms

Optical Components

Equipment

Solar Arrays Structures & Mechanisms

Electronics & Sensors

Formosat-5 ICARUS M2Space

GRACE FO LRI MERLIN FRU QT Instruments

Solar ArraysGK2, FS5, S5P, Space IL, NGSAR, EUCLID, IMECE, Vigoride, YORK, NAOS…

StructuresFormosat-5GRACE FO,BepiColombo,…

MechanismsJUICE, Sentinel 5, GFO, GK2, FS5,S5P, OneWeb

El. & SensorsGK2, MERLIN, GFO, Sent. 2, Sent. 6, NGSAR

DEOS

LISA/NGGM

730.01.2020

Clean Rooms

ISO 8 / class 100,000

ISO 7 / class 10,000

ISO 5 / class 100

Manufacturing

Electronics Lab

Laser-optics Lab

Mechanical Workshops

Mechanical Integration

CFRP Production

Test Facilities

Thermal Vacuum Chambers

Temperature Cabinets

Shakers & Shock Tables

PortalTV Chamber

Filament Winding

Hot pressCycling.chamber

CNC MillingCNC TurningOptics Lab

Facilities

8

Org

anig

ram

Company Organization

9

Executive BoardW. Pitz (CEO), B. Doll, F. Gilles

Mechanical EngineeringM. Herding

Subsystem EngineeringJ. Krieger

Mission SuccessN. Beller

AIT and FacilitiesN. Siam

Sen

ior

Expe

rts

neonsee GmbHSTI Share: 62%

Business DevelopmentK. Nicklaus

Finance, Administration & ITF. Gilles Payloads &

Payload Products

K. Voss

Systems & System

ProductsW. Pitz

ElectricalProductsJ. Krieger

Solar Array ProductsE. Ferrando

Solar Array FactoryT. Franck

CarboSpaceTech GmbHSTI Share: 66%

STI develops small satellites and missions, providing low cost solutions for a wide range of applications.

Mis

sio

ns

& S

ate

llite

s

Formosat 5

“Satellite Kit”

Sys. Engineering support, procurement

Structure, solar array, propulsion, sun sensor

Launched in 08/2017

DEOS

Phase A prime, Phase B Client prime

Mission/satellite design

Design of the docking/berthing mechanism

Mission stopped by DLR after Phase B

ICARUS

Tracking of animals from space

ISS payload, attached to Russian module

Launched in 02/2018

In Science operation

First in-orbit-operation of a massive-user – low-energy-device IOT

Small Satellites & Missions

10

12

STI develops optical systems with a focus on earth observation and science missions. Laser metrology

Frequency references

QT Instruments

Structures & Mechanisms

Op

tica

l In

stru

me

nts GRACE Follow-On LRI

Prime for German Laser Ranging Interferometer part

Cooperation with JPL/NASA

Launched 5/2018

MERLIN Frequency Reference Unit

German-French mission on methane gas measurement

Subsystem for absolute frequency reference

FM delivery in 2021

High Stability Laser

Laser system for NGGM, GRACE 2, LISA…

EBB completed, component qualification running

Laser Interferometer Space Antenna

STI selected by ESA as prime for the development the LISA Laser (Phase 1: BB, Phase 2: EM)

WDM for optical communication

2-channel optical communication testbed

Laser Instrument Activities - Overview

30.01.2020

13

STI develops solar array wings Body mounted to multi hinge

deployments

In-house panel manufacturing

Automated cell laydown (since 2018)

26 missions, 9 delivered,5 in orbit, 17 in development

Sate

llite

Equ

ipm

en

tSolar Arrays

Deployable Solar Arrays, external Cell Laydown

GökTürk 2, launched 2012

Formosat-5, launched 2017

Sentinel-5 Precursor, launched 2017

C-Sat, delivered 2017

JASON CS /Sentinel-6, 1st delivered 2019

Body mounted Solar Arrays, external Cell Laydown

Space IL, launched February 2019

NGSAR, delivered 2018

EUCLID, sunshield & SA, delivery 2020

Solar Arrays with automated Cell Laydown by STI

Lapan A4(Indonesia), delivered 2019

York Space Systems, launched 5/2019 - single Hinge

Imece, deployable solar array, delivery 2020 -single Hinge

Vigoride, delivered 2020 - multi-hinge

NAOS, delivery 2020 - multi-Hinge

12 Solar arrays for Copernicus HPCM: CHIME, CO2M, CRISTAL, LSTM, until 2028

FLEX, ALTIUS, YORK, CO3D, PLATO (PVA),…

York

S-5p

GK2 FS-5

Beresheet

LAPAN A4

Vigoride

NAOS

30.01.2020

14

STI develops reliable and robust deployment mechanisms Robust & lightweight

mechanisms

CFRP Integrated hinge technology

New Space solutions

Sate

llite

Equ

ipm

en

tDeployment Mechanisms

Solar Array Deployment Mechanisms

Kompsat-3, Cam system, CFRP-strut, launched 2012

Göktürk-2, Cam system, no strut, launched 2012

Sentinel-5, Cam system, CFRP-strut, launched 2017

C-Sat, all CFRP strut, delivered 2017

Jason-CS/Sentinel-6, delivered 2019

Vigoride, multi-hinge (4 panels + Yoke), delivery 2020

NAOS, multi hinge (2 panels), delivery 2020

Deployable Antennas

GRACE FO S-Band Antenna, cam system, launched 2018

JUICE RIME antenna, multi hinge, all CFRP hinges, ultra lightweight, 16 m, 1.4 kg

Envision SRS Boom (Phase A/B1)

Airbus Oneweb Satellites SADM

un-synchronized multi-hinge design

80 launched, > 600 delivered, 1200 in production

30.01.2020

STI develops structures, mechanisms & MGSE for most demanding missions. In-House metal & CFRP

manufacturing facilities

Sate

llite

Equ

ipm

en

t

Formosat-5

Primary structure, top panel, MGSE

Delivered 2012/2013

Launched August 2017

GRACE Follow-on

Primary and secondary structure, MGSE

Deployable S-Band antenna boom

Delivered 2015/2016

Launched May 2018

Refocus Mechanisms (BB tests completed)

Motor driven (0.5 µm accuracy, 300µm travel)

Heater driven (0.5 µm accuracy, 10µm travel)

In development (C/D contract)

Sentinel-5 Calibration Subsystem (CAS)

BIOMASS MGSE

Structures, mechanisms & MGSE

15

STI develops sensors & electronics with a focus on: Instrument control units

Remote terminal Units

Ultra low noise current sources

Safe mode AOCS Sensors

Sate

llite

Equ

ipm

en

t

CESS

< 12° peak error on Earth vector

< 5° peak error on Sun vector

Supports spin rates up to 10°/s

On 15 missions in Orbit

GökTürk 2

Pyrodrive Module

Launched 2012

Satellite Core Avionics

Combination of OBC and PCDU for small satellites

Prototype demonstrated 2015

MERLIN Frequency Reference Unit

FRU control electronics, FPGA based

FM delivery scheduled for 2018

Laser Diode Drivers

Ultra low noise current sources

For use with e.g. DFB & ECDL Lasers

Remote Terminal Units

Dual Core LEON3 processor

Remote data concentrator EQM

RCSMTMT

3-axisGPSGPS

CESS /

OSS

AOCS Equipment

ThermHeater

Thermal Ctrl. Equip.

SCSCCESS /

OSSCESS

6 heads

AOCS SensorsAOCS ActuatorsHead

Head

RCSRCS

3 branches A, B, C

HeaterHeater ThermTherm

3 groups A, B, C

EGSESA Generator Battery S-Band RFEA

Cold/hot redundant

functional redundant

Satellite Core

Avionics

CAN-Bus B

Umbilical /

Test IF

SPC Module N

(SCOC3)

Pwr

POL

Pwr IF

CA int. PWR A

CA int. PWR B

CAN-Bus A

Ctrl B

Ctrl A

CAN A CAN B

SPC Module R(SCOC3)

CAN A CAN B

Pwr

POL

TX TXRX RX

TMTCTMTC

I/O Module A

RCS A

CESS A

SC A

MT A

Payload A

Heater A

Therm A

I/O Module B

RCS B

CESS B

SC B

GPS A

Payload B

Heater B

Therm B

I/O Module C

RCS C

CESS C

GPS B

MT B

Heater C

Therm C

Ctrl

CAN A CAN B

Ctrl

CAN A CAN B

Ctrl

CAN A CAN B

SC A, B GPS A, BCESS A, B, CHeater A, B, C Therm A, B, C MT A, B RCS A, B, C

CAN-bus

I/F =

CAN-bus or

UART or Spacewire

Primary Power

Int.Power to I/O

Modules 3x

Pwr

POL

Pwr

POL

Pwr

POL

Nominal Redundant

4xR

FE

A

3-6

x N

EA

2xG

PS

2x S

C

4xP

aylo

ad

Payload / Instrument

IF A IF BIF A IF B

DCDC

A

DCDC

B

PCDU Modules- Charge control

- Battery / Power Bus IF

- Pwr Bus Filter

- Power Distribution (LCL)

- Special. Actuation outlets

- Pwr Status / Monitoring

- DC/DC external supply

LCL, switches

SAR

(MPPT)

Battery

IF

PWR Bus

Filter

Electronics

16

17

Faci

litie

s

12 000 m2 STI Site

Present

2020: new building G4for Solar Array Factory, STI and CST offices

2022+: new buildings G5 and G6EV Tests and Cleanroom, STI and CST offices

STI Site & Site Extension Plan

Thank you very muchfor your attention!

SpaceTech GmbH

Systems

Instruments

Equipment

Seelbachstr. 13 D-88090 ImmenstaadTel: +49 7545 932 84 86 www.spacetech-i.com

12.11.2020