- Overall dimensions (without
antennas) 320 x 340 x 362 [mm]
- Power:
- 4 Solar Panels, 320 x 320
mm, 34 cells in series, max. 14 W each
- 4 NiH2 Batteries,
10V nominal voltage, 12 Ah
- PCU for power control,
conditioning and distribution
- electronic fuses and
latch-up protection
- Communication
- TTC1 in UHF, Modulation FFSK,
1200/2400 Baud, 3.5 W RF output
- TTC2 in VHF, Modulation FFSK,
1200/2400 Baud, 5.0 W RF output
- CRC and FEC check
- Data handling and processing
- OBDH with 256 kB static RAM,
128 kB EEProm, 64kB ROM
- Model Calculator with 512 kB
RAM, 256 kB EEprom, 64kB ROM
- SEU protection
- Attitude Control System
- 3 Wheel / Gyro couples in
orthogonal axes
- Star Sensor for 3 axes
inertial attitude determination
- 3 axes magnetic field sensor
- magnetic coil in X axes
- single solar cells for sun
determination (emergency/coarse mode)
- S-Band Transmitter with patch
antenna
- Modulation BPSK, FEC, max
250 kBaud, 2.0 W RF output
- Camera
- CCD Matrix Array, 770 x 576
Pixel, Pixelsize 32.5 µm
- optics: focal length 72 mm,
f/number 6
- FOV ca. 8 °
- filter for near infrared
- nominal integration time 28
ms
- digital resolution 12 Bit
- Payload data handling
- Frame Data Handling System
- Messaging system for store and
forward communication
| Maroc-Tubsat
|
|
SPACECRAFT
|
| Int'l Designation |
|
Launched
|
| Owner / Sponsor |
Royal
Center for Remote Sensing (Morocco)
|
| Mission |
Technology
|
| Satellite Bus |
Technical
University of Berlin
|
Tubsat C
|
| Launch Mass |
45 kg (99 lbm)
|
| Mission Orbit |
SSO
|
°
|
| Design Life |
|
| Power (EOL) |
|
|
LAUNCH
|
| Launch Vehicle
Model |
Zenit
2 |
| Launch Date / Time |
2001
December 10
|
17:19
|
| Co-Passenger(s) |
Meteor
3M-N1 |
| |
Badr
B |
| |
KOMPASS
|
| |
Reflektor |
|
FINANCIAL
|
| Satellite cost |
|
| Web Links |
Tubsat
Link
|
|
|
