All rights reserved, 2007, Thales Alenia Space EXOMARS Industry Day Carrier Module Presentation...
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Transcript of All rights reserved, 2007, Thales Alenia Space EXOMARS Industry Day Carrier Module Presentation...
All rights reserved, 2007, Thales Alenia Space
EXOMARS Industry Day
Carrier Module PresentationThales Alenia Space- Italia (Turin)
All rights reserved, 2007, Thales Alenia Space
Page 2
CM Overview
Carrier Module
(including DM on top)
All rights reserved, 2007, Thales Alenia Space
Page 3
CM Product Tree
Carrier Product tree
Carrier Module
PCA & PIA units
424N Engine
10N Thrusters
MON Tank
Miscellaneous
Propulsion
CSS
STR
GNC
TAS-F
OHB
HGA
X-DST
TT&C
TWTA
LGAs
RFDN
E 11
Carrier AER system
E 111
Carrier AER system
E 111
Carrier MTP system E 112
Carrier MTP system E 112
E 1113
E 1114
PCDU
Battery
Power
Harness assy
E 1111
E 11111
E 11112
E 11113
PCDU
Battery
Power
Harness assy
E 1111
E 11111
E 11112
E 11113
Solar ArrayE 1112
Structural PanelE 11121
Structural PanelE 11121
Mechanisms E 11122Mechanisms E 11122
E 11131
E 11132
Tubing assy
E 1124
Thermal Control
E 1123
Thermal ControlThermal Control
E 1123
Structure assyE 1121
Structure assyE 1121
TPA
E 11141
E 11142
E 11143
E 11144
E 11145
E 11146
Central TubeE 11211
Central TubeE 11211
StructuresE 11212
StructuresE 11212
220N EnginesMiscellaneousE 11213
MiscellaneousE 11213
E 11241
E 11242
E 11243
E 11244
E 11245
MMH Tanks
He TanksE 11246
E 11247
E 11248
E 11249
Data Handling
RTU
E 1115
E 11151
Data Handling
RTU
E 1115
E 11151
Photo Voltaic Assy E 11123
Photo Voltaic Assy E 11123
All rights reserved, 2007, Thales Alenia Space
Page 4
CM Procurement List
MTP Structure Central TubeStructures (Panels & second. struct.)
Thermal Control Hardware (MLI)
Propulsion Units:• 424N Main Engine • 220N back-up for main engine.• 10N Thrusters• He tanks• MON Tank • MMH
MTD units
MGSE
AERPCDU/RTUBatteryHarnessSolar Array Panels and PVASTRCSSA
TTC Units:• HGA• LGA• TPA (TBC)• X DST• TWTA• RFDN
EGSE
All rights reserved, 2007, Thales Alenia Space
Page 5
CM Mechanical
Central Tube1 194 mm diameter tube
2 260 mm Height
ITT issued in April
Propositions received
Waiting for sub-co selection
J A S O N D J F M A M J J A S O N D J F M A M J J A S O N D J F M A7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40
Central tube STM
PFM
2011
Equipment
2008 2009 2010
All rights reserved, 2007, Thales Alenia Space
Page 6
CM Mechanical
StructuresPanels associated to the Central Tube
CFRP panels
J A S O N D J F M A M J J A S O N D J F M A M J J A S O N D J F M A7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40
Panels and Structures
2008 2009 2010 2011
Equipment
All rights reserved, 2007, Thales Alenia Space
Page 7
CM Mechanical
MTD• Mechanical Thermal Dummies• Simplified unit box representatives of the Mass, size, foot print and fixation, emissivity, thermal dissipation (heaters)• 10 units
J A S O N D J F M A M J J A S O N D J F M A M J J A S O N D J F M A7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40
MTD
2008 2009 2010 2011
Equipment
All rights reserved, 2007, Thales Alenia Space
Page 8
CM Propulsion units
1 x MON Tank 1194 diameter, 1 450 litres
4 x MMH Tanks 600 diameter, 406 litres
1 x Main Engine 424N
2 x 220N Thrusters (ATV)
12 x 10N Thrusters
J A S O N D J F M A M J J A S O N D J F M A M J J A S O N D J F M A7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40
Central Tank (MON)
External Tanks (MMH)
He Tanks
424N engine
220N thrusters
10N thrusters
2008 2009 2010 2011
Equipment
All rights reserved, 2007, Thales Alenia Space
Page 9
CM Thermal Control
MLI
• Internal MLI• External MLI• High temperature MLI around thrusters and Main Engine
J A S O N D J F M A M J J A S O N D J F M A M J J A S O N D J F M A7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40
Thermal Control H/W
2008 2009 2010 2011
Equipment
All rights reserved, 2007, Thales Alenia Space
Page 10
CM MGSE
MGSE-CTCBContainer
MGSE-CIHT,CVIS,CVHD,CHTA
J A S O N D J F M A M J J A S O N D J F M A M J J A S O N D J F M A7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40
MGSE-CTCB
MGSE-CIHT,CVIS,CVHD,CHTA
2008 2009 2010 2011
Equipment
All rights reserved, 2007, Thales Alenia Space
Page 11
CM PCDU
Power Conditioning and Distribution Unit (PCDU)•power distribution,•GNC & RCS management,•standard I/O. The PCDU will include the following modules and functions :
•PCU : provides a 22-34V unregulated bus, based on a Maximum Power Point Tracking (MPPT) regulator topology. The input power will be delivered from a SA during sunlight periods, or from a Li-Ion battery during eclipses and when the SA power is lower than the power demand.
•PDU : distributes protected lines to DM, CM units & heaters, and commands pyro devices,
•RTU : assures GNC/RCS interfaces, delivers Standards I/O.
All rights reserved, 2007, Thales Alenia Space
Page 12
CM PCDU
PCDU block diagram
Bus22-34V
CMBTY
CM PCDU
PCU PDU
CMUMB IF
RTU
CDMU
SA
Cbus
1553 Bus (A&B)
PCDU DTC&DTM
Secondary ground
Mechanical ground
DM PCDU
Pyros
TCS
STR
CSS
RCSunits
I/F CM I/F DM
DTC/DTM
Separation strap & UMB
I/O
Power N&R (*)
Primary ground
(*) Insulated lines
X-DST
TWTA
J A S O N D J F M A M J J A S O N D J F M A M J J A S O N D J F M A7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40
PCDU/RTU
2008 2009 2010 2011
Equipment
All rights reserved, 2007, Thales Alenia Space
Page 13
CM Battery
Battery• Technology: Lithium-Ion• Bus voltage: 20 - 34V• Name plate capacity: 80 Ah (TBC)• Lifetime: 2 years storage / 36 months in orbit (less than 100
cycles , max DOD 80% )• Mass 20 Kg
J A S O N D J F M A M J J A S O N D J F M A M J J A S O N D J F M A7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40
Battery
2008 2009 2010 2011
Equipment
All rights reserved, 2007, Thales Alenia Space
Page 14
CM Harness
Harness• Power, Signals and 1553• Roughtly 6 500 points / 250 connectors• Mass: 30 Kg
J A S O N D J F M A M J J A S O N D J F M A M J J A S O N D J F M A7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40
Harness
2008 2009 2010 2011
Equipment
All rights reserved, 2007, Thales Alenia Space
Page 15
CM Solar Array H/W
Solar Array Panels• 2 structural CFRP panels • 2 x 4.5 m²
Solar Array PVA• Photo Voltaic Assy of 1 800 W at 1 AU• AsGa cells• Mars Orbiting at 1.6 AU
J A S O N D J F M A M J J A S O N D J F M A M J J A S O N D J F M A7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40
SA panels
SA PVA
2008 2009 2010 2011
Equipment
All rights reserved, 2007, Thales Alenia Space
Page 16
CM GNC
2 x STR• 3-axis autonomous acquisition and tracking w/o any rate
information• The tracking shall be robust to angular rate up to 1,5 deg/sec.• The tracking shall be robust to the Solar flare.• The autonomous acquisition shall be performed within 10 minutes
in the presence of TBD false star in the field of view.
1 x CSSA• Core Sun Sensor Assembly
J A S O N D J F M A M J J A S O N D J F M A M J J A S O N D J F M A7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40
STR
CSSA
2008 2009 2010 2011
Equipment
All rights reserved, 2007, Thales Alenia Space
Page 17
CM TTC &RF
2 X-DST, X band Deep Space Transponders. (Used to acquire, lock and demodulate the Rx signal in X band, to synchronize, generate and modulate the Tx signal in X band and to transpond ranging signals. Compatible with DDOR and )
2 TWTA : X band Travelling Wave Tube Assembly, 65W RF output power.(Used to amplify the signal)
1 RFDN : X band RF Distribution Network (provides connection between antennas and Rx or TWTA), including mainly diplexers and switches.
1 HGA, X band High Gain Antenna : baseline is a single offset reflector antenna (diameter 1100mm) ; Tx gain ~34.4dBi ; Rx gain 33.4 dBi ; circular polarisation
3 LGA, X band Low Gain Antenna : omni-directional antenna based on a chocked horn , circular polarisation. (Tx gain >-3dBi ; Rx gain >-2dBi dBi within 90°)
TPA (TBC) Xband Toroidal Pattern Antenna
J A S O N D J F M A M J J A S O N D J F M A M J J A S O N D J F M A7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40
X band transponder
TWTA
HGA
X band LGA
RFDN
Equipment
2008 2009 2010 2011
All rights reserved, 2007, Thales Alenia Space
Page 18
CM EGSE
ATB + AIT EGSE
J A S O N D J F M A M J J A S O N D J F M A M J J A S O N D J F M A7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40
ATB + AIT EGSE
2011
Equipment
2008 2009 2010
CCS
TM/TC FEE
Pow er FEE
Data Handling SCOE
AOCS SCOE
STR EGSE
STR OGSE
Pow er SCOE ( & OTS..)
1553 Emulator
TTC RF SCOE
ATB CM Harness