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

Timestamp:

11/05/18 07:00:32 (6 years ago)

Author:

Mehr Mohammad Sachal

Comment:

--

UserApp/Proba-V

@@ -164 +164 @@
 
 
-|| '''Overview of PROBA-V subsystems''' ||
- 
-|| 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''' || 
-||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''' ||
-||Bus structure||Aluminum (AA2024-T3);Aluminum (AA7075-T7351);3 CFRP (EX-1515/M55J + Redux 312L) outer panels|| 
-||'''New development''' || 
-||AOCS actuators ||3 magnetotorquers (internally cold redundant); 4 reaction wheels (3 + 1 for redundancy); 2 magnetometers (cold redundant)||
-||'''ROBA-2/PROBA-1'''||
-||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'''|| 
-||Onboard SW||Operating System: RTEMS (Real-Time Executive for Multiprocessor Systems)|| 
-||'''PROBA-2'''|| 
-||Thermal||Passive (MLI and paint)|| 
-||RF communications||S-band TxRx : 5W BPSK; X-band Tx: 6 W filtered OQPSK; MMU (Mass Memory Unit) = 16 Gbit|| 
-
-
-
-||'''PROBA-V spacecraft accommodation (image credit: QinetiQ Space)'''||
-||[[Image(wiki:File:ProbaV_Auto10.jpeg File:ProbaV Auto10.jpeg)]]||
+'''Overview of PROBA-V subsystems'''
+
+||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||
+||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||
+||Bus structure||Aluminum (AA2024-T3);Aluminum (AA7075-T7351);3 CFRP (EX-1515/M55J + Redux 312L) outer panels||New development||
+||AOCS actuators||3 magnetotorquers (internally cold redundant); 4 reaction wheels (3 + 1 for redundancy); 2 magnetometers (cold redundant||ROBA-2/PROBA-1
+||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
+||Onboard SW||Operating System: RTEMS (Real-Time Executive for Multiprocessor Systems)||PROBA-2||
+||Thermal||Passive (MLI and paint)|| ||
+||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|| 
+
+
+
+ ||'''PROBA-V spacecraft accommodation (image credit: QinetiQ Space)'''||
+ ||[[Image(wiki:File:ProbaV_Auto10.jpeg File:ProbaV Auto10.jpeg)]]||
 
 == AOCS (Attitude and Orbit Control Subsystem)  ==