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Launch your Vision Company Presentation€¦ · Company Portfolio & Heritage examples ... Overview...
Transcript of Launch your Vision Company Presentation€¦ · Company Portfolio & Heritage examples ... Overview...
Company Presentation
SpaceTech GmbH
Launch your Vision
In Orbit on 10 Missions 50 Satellites 107 Equipments
York
GFO
S-5P
K-3
OneWeb
FS-5
S2
Space IL
ICARUS
In Orbit on 10 Missions 50 Satellites 107 Equipments
Developments for 15 Missions 882 Satellites 1751 Equipments
OneWeb
IMECE
York
LAPAN A4
MERLIN
S5
C-SAT
JUICE
JASON/S6
NGSAR
EUCLID
GFO
S-5P
GK-2
K-3
OneWeb
FS-5
S2
Space IL
ICARUS
NAOS
Vigoride
WDM
In Orbit on 10 Missions 50 Satellites 107 Equipments
Developments for 15 Missions 882 Satellites 1751 Equipments
And more to come …
NGGM
LISA
M2Spacee
G2G
HRWS
iBOSS
OneWeb
IMECE
York
LAPAN A4
MERLIN
S5
C-SAT
JUICE
JASON/S6
NGSAR
EUCLID
GFO
S-5P
GK-2
K-3
OneWeb
FS-5
S2
Space IL
ICARUS
NAOS
Vigoride
Spacedrone23.10.2019 4
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
Mechanical Engineering
Subsystem Engineering(SA/ Laser, Optics, El., S/W)
Mission Success
AIT and Facilities
Executive BoardW. Pitz (CEO), B. Doll, F. Gilles
SystemsW. Pitz
Solar Arrays & Mechanical
ProductsT. Franck
ElectricalProductsJ. Krieger
PayloadsK. Voss
Finance, Administration & ITF. Gilles
Business DevelopmentK. Nicklaus
Carbospacetech GmbH66% STI Share
Sen
ior
Expe
rts
neonsee GmbH62% STI Share
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)
13 missions, 9 delivered,5 in orbit, 4 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
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