Changes between Version 37 and Version 38 of UserApp/Proba-V


Ignore:
Timestamp:
Nov 5, 2018, 7:00:32 AM (8 months ago)
Author:
Mehr Mohammad Sachal
Comment:

--

Legend:

Unmodified
Added
Removed
Modified
  • UserApp/Proba-V

    v37 v38  
    164164
    165165
    166 || '''Overview of PROBA-V subsystems''' ||
    167  
    168 || Avionics ||||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 ||
    169 ||'''PROBA-2 ; New development''' ||
    170 ||EPS (Electric Power Subsystem)||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||
    171 ||'''Herschel; PROBA-1''' ||
    172 ||Bus structure||Aluminum (AA2024-T3);Aluminum (AA7075-T7351);3 CFRP (EX-1515/M55J + Redux 312L) outer panels||
    173 ||'''New development''' ||
    174 ||AOCS actuators ||3 magnetotorquers (internally cold redundant); 4 reaction wheels (3 + 1 for redundancy); 2 magnetometers (cold redundant)||
    175 ||'''ROBA-2/PROBA-1'''||
    176 ||AOCS sensors ||2 star trackers; 2 GPS (cold redundant); AOCS IF box (internally redundant); RW Power Supply box (internally redundant)||
    177 ||'''PROBA-1/-2; New development'''||
    178 ||Onboard SW||Operating System: RTEMS (Real-Time Executive for Multiprocessor Systems)||
    179 ||'''PROBA-2'''||
    180 ||Thermal||Passive (MLI and paint)||
    181 ||RF communications||S-band TxRx : 5W BPSK; X-band Tx: 6 W filtered OQPSK; MMU (Mass Memory Unit) = 16 Gbit||
    182 
    183 
    184 
    185 ||'''PROBA-V spacecraft accommodation (image credit: QinetiQ Space)'''||
    186 ||[[Image(wiki:File:ProbaV_Auto10.jpeg File:ProbaV Auto10.jpeg)]]||
     166'''Overview of PROBA-V subsystems'''
     167
     168||Avionics||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||PROBA-2 ; New development||
     169||EPS (Electric Power Subsystem||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||Herschel; PROBA-1||
     170||Bus structure||Aluminum (AA2024-T3);Aluminum (AA7075-T7351);3 CFRP (EX-1515/M55J + Redux 312L) outer panels||New development||
     171||AOCS actuators||3 magnetotorquers (internally cold redundant); 4 reaction wheels (3 + 1 for redundancy); 2 magnetometers (cold redundant||ROBA-2/PROBA-1
     172||AOCS sensors||2 star trackers; 2 GPS (cold redundant); AOCS IF box (internally redundant); RW Power Supply box (internally redundant)||PROBA-1/-2; New development
     173||Onboard SW||Operating System: RTEMS (Real-Time Executive for Multiprocessor Systems)||PROBA-2||
     174||Thermal||Passive (MLI and paint)|| ||
     175||RF communications||S-band TxRx: 5W BPSK; X-band Tx: 6 W filtered OQPSK; MMU (Mass Memory Unit) = 16 Gbit||PROBA-1/-2; ; New development||
     176
     177
     178
     179 ||'''PROBA-V spacecraft accommodation (image credit: QinetiQ Space)'''||
     180 ||[[Image(wiki:File:ProbaV_Auto10.jpeg File:ProbaV Auto10.jpeg)]]||
    187181
    188182== AOCS (Attitude and Orbit Control Subsystem)  ==