[FONT=Arial CE,sans-serif][SIZE=+1]MAROC-TUBSAT[/SIZE][/FONT][FONT=Arial CE,sans-serif]The Project[/FONT][FONT=Arial CE,sans-serif][SIZE=-1]The MAROC-TUBSAT project is a cooperation between CRTS Morocco and the Institut für Luft-und Raumfahrttechnik in Berlin, where the Moroccan side is responsible for payload and launch and the German side for the satellite bus.[/SIZE][/FONT][FONT=Arial CE,sans-serif][SIZE=-1]The main tasks of the satellite are Earth remote sensing and vegetation detection with a medium resolution of about 300 m, store and forward communications for mobile localization and developing attitude control strategies for high resolution earth observation.[/SIZE][/FONT][FONT=Arial CE,sans-serif]Technical Characteristics[/FONT][FONT=Arial CE,sans-serif][SIZE=-1]More information: [/SIZE][/FONT][FONT=Arial CE,sans-serif][SIZE=-1]ILR, TU-Berlin[/SIZE][/FONT]
- [FONT=Arial CE,sans-serif][SIZE=-1]Overall mass: 47 kg[/SIZE][/FONT]
- [FONT=Arial CE,sans-serif][SIZE=-1]Overall dimensions (without antennas) 320 x 340 x 362 [mm][/SIZE][/FONT]
- [FONT=Arial CE,sans-serif][SIZE=-1]Power:[/SIZE][/FONT]
- [FONT=Arial CE,sans-serif][SIZE=-1]4 Solar Panels, 320 x 320 mm, 34 cells in series, max. 14 W each[/SIZE][/FONT]
- [FONT=Arial CE,sans-serif][SIZE=-1]4 NiH2 Batteries, 10V nominal voltage, 12 Ah[/SIZE][/FONT]
- [FONT=Arial CE,sans-serif][SIZE=-1]PCU for power control, conditioning and distribution[/SIZE][/FONT]
- [FONT=Arial CE,sans-serif][SIZE=-1]electronic fuses and latch-up protection
[/SIZE][/FONT]- [FONT=Arial CE,sans-serif][SIZE=-1]Communication[/SIZE][/FONT]
- [FONT=Arial CE,sans-serif][SIZE=-1]TTC1 in UHF, Modulation FFSK, 1200/2400 Baud, 3.5 W RF output[/SIZE][/FONT]
- [FONT=Arial CE,sans-serif][SIZE=-1]TTC2 in VHF, Modulation FFSK, 1200/2400 Baud, 5.0 W RF output[/SIZE][/FONT]
- [FONT=Arial CE,sans-serif][SIZE=-1]CRC and FEC check
[/SIZE][/FONT]- [FONT=Arial CE,sans-serif][SIZE=-1]Data handling and processing[/SIZE][/FONT]
- [FONT=Arial CE,sans-serif][SIZE=-1]OBDH with 256 kB static RAM, 128 kB EEProm, 64kB ROM[/SIZE][/FONT]
- [FONT=Arial CE,sans-serif][SIZE=-1]Model Calculator with 512 kB RAM, 256 kB EEprom, 64kB ROM[/SIZE][/FONT]
- [FONT=Arial CE,sans-serif][SIZE=-1]SEU protection
[/SIZE][/FONT]- [FONT=Arial CE,sans-serif][SIZE=-1]Attitude Control System[/SIZE][/FONT]
- [FONT=Arial CE,sans-serif][SIZE=-1]3 Wheel / Gyro couples in orthogonal axes[/SIZE][/FONT]
- [FONT=Arial CE,sans-serif][SIZE=-1]Star Sensor for 3 axes inertial attitude determination[/SIZE][/FONT]
- [FONT=Arial CE,sans-serif][SIZE=-1]3 axes magnetic field sensor[/SIZE][/FONT]
- [FONT=Arial CE,sans-serif][SIZE=-1]magnetic coil in X axes[/SIZE][/FONT]
- [FONT=Arial CE,sans-serif][SIZE=-1]single solar cells for sun determination (emergency/coarse mode)
[/SIZE][/FONT]- [FONT=Arial CE,sans-serif][SIZE=-1]S-Band Transmitter with patch antenna[/SIZE][/FONT]
- [FONT=Arial CE,sans-serif][SIZE=-1]Modulation BPSK, FEC, max 250 kBaud, 2.0 W RF output
[/SIZE][/FONT]- [FONT=Arial CE,sans-serif][SIZE=-1]Camera [/SIZE][/FONT]
- [FONT=Arial CE,sans-serif][SIZE=-1]CCD Matrix Array, 770 x 576 Pixel, Pixelsize 32.5 µm[/SIZE][/FONT]
- [FONT=Arial CE,sans-serif][SIZE=-1]optics: focal length 72 mm, f/number 6[/SIZE][/FONT]
- [FONT=Arial CE,sans-serif][SIZE=-1]FOV ca. 8 °[/SIZE][/FONT]
- [FONT=Arial CE,sans-serif][SIZE=-1]filter for near infrared[/SIZE][/FONT]
- [FONT=Arial CE,sans-serif][SIZE=-1]nominal integration time 28 ms[/SIZE][/FONT]
- [FONT=Arial CE,sans-serif][SIZE=-1]digital resolution 12 Bit
[/SIZE][/FONT]- [FONT=Arial CE,sans-serif][SIZE=-1]Payload data handling[/SIZE][/FONT]
- [FONT=Arial CE,sans-serif][SIZE=-1]Frame Data Handling System
[/SIZE][/FONT]- [FONT=Arial CE,sans-serif][SIZE=-1]Messaging system for store and forward communication[/SIZE][/FONT]
[FONT=Arial CE,sans-serif][SIZE=-1]MAROC-TUBSAT was launched with a Zenit rocket on the 10th of December in 2001 into a sun-synchronous orbit with an altitude of 1000 km from the Baikonur Cosmodrome. Three years after launch, the satellite is still complete operational.[/SIZE][/FONT][FONT=Arial CE,sans-serif][SIZE=-1]German Team:
Project Manager: P. Butz (1995-2000 TU-Berlin)[/SIZE][/FONT]
http://www.vectronic-aerospace.com/html/maroc-tubsat.html