- Timestamp:
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12/04/11 14:17:10 (13 years ago)
- Author:
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Iliyankatsarski
- Comment:
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Legend:
- Unmodified
- Added
- Removed
- Modified
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v7
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v8
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129 | 129 | |
130 | 130 | The power distribution and conditioning part of ADPMS supplies an unregulated bus, with each equipment having its internal DC/DC converter. The power conditioning system is designed around a Li-ion battery. |
| 131 | |
| 132 | |
| 133 | {| border="1" |
| 134 | |+ '''Table 1: Overview of PROBA-V subsystems''' |
| 135 | |- |
| 136 | |Avionics |
| 137 | |ADPMS (cold redundant),MPM (Main Processor Module): LEON2-E Sparc V8 processor, 50 MHz,42 MIPS, 10 FLOPS,Mass memory Module: 16 Gbit Flash, EDAC protected |
| 138 | |PROBA-2 ; New development |
| 139 | |- |
| 140 | |EPS (Electric Power Subsystem |
| 141 | |Photo-Voltaic Array : Triple junction GaAs cells; Cover glass CMG 100AR coating, 25 strings, 18 cells per string;Battery:12 Ah Li-ion (7s8p) ABSL 18650HC cells |
| 142 | |Herschel; PROBA-1 |
| 143 | |- |
| 144 | |Bus structure |
| 145 | |Aluminum (AA2024-T3);Aluminum (AA7075-T7351);3 CFRP (EX-1515/M55J + Redux 312L) outer panels |
| 146 | |New development |
| 147 | |- |
| 148 | |AOCS actuators |
| 149 | |3 magnetotorquers (internally cold redundant); 4 reaction wheels (3 + 1 for redundancy); 2 magnetometers (cold redundant |
| 150 | |ROBA-2/PROBA-1 |
| 151 | |- |
| 152 | |AOCS sensors |
| 153 | |2 star trackers; 2 GPS (cold redundant); AOCS IF box (internally redundant); RW Power Supply box (internally redundant) |
| 154 | |PROBA-1/-2; New development |
| 155 | |- |
| 156 | |Onboard SW |
| 157 | |Operating System: RTEMS (Real-Time Executive for Multiprocessor Systems) |
| 158 | |PROBA-2 |
| 159 | |- |
| 160 | |Thermal |
| 161 | |Passive (MLI and paint) |
| 162 | | |
| 163 | |- |
| 164 | |RF communications |
| 165 | |S-band TxRx: 5W BPSK; X-band Tx: 6 W filtered OQPSK; MMU (Mass Memory Unit) = 16 Gbit |
| 166 | |PROBA-1/-2; ; New development |
| 167 | |} |
131 | 168 | |
132 | 169 | |