2006/3/22 5-3-1 system block diagram mechanical interface and component layout power distribution...
TRANSCRIPT
2006/3/22 5-3-1
System Block Diagram
Mechanical Interface and Component Layout
Power Distribution
Major Subsystem Status
2006/3/22 5-3-2
System Block Diagram
DR
DMC
SSC
Normal Heater
SSAS-S×2
SASA
APR
: Signal
XDIP-A
XSW-A
XDIP-B
XSW-B
TWTA
TRP-A
TRP-B
XSW-C(DPDT
)
HGA
APM
RF S/STLM/CM
DRUADM
2ndPWR
ND
RJ
from/to ADM
SEPM/CPM/MPO
Power Source
MGA
from/to APM
MIA
MSA
MEA2
MEA1
HEP-i
HEP-e
ENA
MSASI
MDM
MGF-OMGF-IMAST-MGFPWI-SC MAST-SC
: RF
: SpaceWire DS link
: Primary Power
: PSU (other box)
CPM/MPOElectronics
SeparationConnector
XSW-C(DPDT
)
MDP-2 DPU PSU IPD
MGF-OMGF-I
PWI EWO SORBET AM2P MEFISTO-EMAST/WPT-E
PWI-WPT
PWI-MEFISTOTWTA
MDP-1 DPU PSU IPD
SpaceWire (A/B)
MIL-STD-1553B (A/B)
SEPM/CPM/MPO
Power Source
To UPG
To UPG
SSAS-E
SEPM/CPM/MPO
Power Source
Connector SeparationMechanism
Spin Ejection MechanismMechanism
CNV2
CNV1
SPM
RCS
P
thruster modulethruster module
valve module
P P
GN2TAN
K
BAT
PCU
IG-PS
PYRO forHGA LatchMechanism
Primary Powerfor S/S
S/S RTN
SW
&
Li
mit
er
BU
S-
BA
T
Sw
itch
: PSU (in the box)
Survival Heater
From PCU
UPG
2006/3/22 5-3-3
Component Layout (1/2)
MIA
HEP-i
(1)
(4)
(5)
(2)
(3)
(6)
(7)
(8)
ENA
MEA2
Upper Thruster Module(2 places)
SSASMSA
MEA1 HEP-e
MAST-SC
MAST-MGF
X
Y
Z
MSASI
Lower Thruster Module(2 places)
MGA (after deployment)
WPT1
MAST-MGF
SSC
WPT2
MEFISTO2 MEFISTO1
MAST-SC
X
Y
Z
Top View Bottom View
2006/3/22 5-3-4
Component Layout (2/2)
Internal Surface of the Upper Deck,Perspective View from +Z direction.
THR-M
THR-M
Tank
Z X
Y
DRU
EPC
TWT
SSAS-E
SSAS-S
X-TRP1
XSW
XSW
XSW
XSW X-TRP2
TWTEPC
XDIP
XDIP
SPM
APR
DMC
Internal Surface of the Lower Deck,Perspective View from +Z direction.
CNV-1
CNV-2
Z X
Y
BAT
MDP1
MDP2
HEP-e
MEA
MAST-MGF
MAST-SC
HEP-i
MIA
MDM
V-M
MSAWPT-Pre
WPT-Pre
SSC
PCU
MSASIMEA
ENA
MDM-S
2006/3/22 5-3-5
Geometrical Interface for instruments
Updating now
Upper Deck
Bulkhead
Substrate Support Fixture
Lower Deck
Substrate
Substrate Support Fixture will be moved tothe exposed side.It will mitigate restriction on instruments mounting at the corner.
Ref. MMO-NT-D05013
2006/3/22 5-3-6
Power Distribution for payloads
Issues and possible resolutions
> Motors for MEFISTO, WPT, and MAST require 28V, not 50V. External PSU to provide 28V power
> Centralized vs. Distributed architecture.It would be too complex to have all of switching functions and secondary power supply functions at the MDP. External PSU for each MPPE and MDM instrument
> How to distribute +3.3V to instruments.It would be difficult to provide such a low voltage with good quality from the external PSU. To generate +3.3V by onboard regulator within instruments
2006/3/22 5-3-7
Alternative Power Distribution Architecture for payloads
PS
U
PS
U
PS
UM
EA
-1
PS
UM
EA
-2
PS
UM
IA
PS
UM
SA
PS
UH
EP
-e
PS
UH
EP
-i
PS
UEN
A
DP
U
MG
F-oe
MS
AS
I
PS
UM
DM
PW
IEW
O
MG
F-oe
PW
IS
OR
BE
TPW
IA
M2
P
PW
IM
EFIS
TO
-EM
AS
T/
WP
T-E
PS
U
PS
UD
PU
MDP-1
MD
P-2
IPD
PC
D
DM
C(A
)D
MC
(B)
DR
U(A
)D
RU
(B)
PC
D(A
)P
CD
(B)
XTR
P-A
XTR
P-B
EP
C-A
EP
C-B
10
lines
for
BU
S
com
p.
PS
U
PS
U