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Chandrayaan-1

Chandrayaan-1 is ISRO's first mission to the Moon. It will be launched in late 2008 on board a Polar Satellite Launch Vehicle from the SDSC launch site in India. It is currently planned that Chandrayaan-1 will take 5.5 days to cruise to the Moon where is will enter into a 100 km circular polar orbit for at least a 2 year science mission.


It has on board 11 instruments. Five of these experiments have been developed in India and the other six experiments have been provided by international partners from the UK, Sweden, Germany, Bulgaria and America.

 

 

C1XS and XSM
The Flight C1XS Instrument in the calibation facility at the Rutherford Appletone Laboratory. IMAGE: RAL

C1XS is a micro-technology demonstrator of a planetary X-ray spectrometer. It is based on the proven heritage of D-CIXS which successfully demonstrated the technological capabilities of this technique when it flew around the Moon on ESAs SMART-1 spacecraft. The accompanying X-ray Solar Monitor (XSM) will study the sun for changes in X-ray flux and X-ray spectrum emission and will be used to calibrate the C1XS lunar data.

The C1XS front end component consists of three facets, all looking in the same direction, with a defined 11 degree FOV (left). Each facet consists of 8 swept charge devices (SCD) X-ray detectors (see below). These detectors are based around e2v technology’s CCD54. Swept Charge Devices are a development on normal X-ray CCD sensors which require much less cooling and have a central read-out channel which takes the collected charge to single output amplifier circuit. The SCDs are mounted behind low profile gold/copper
collimators (a new technological innovation). This combination has the virtue of providing superior X-ray energy resolution in an instrument that is compact and low mass.

 

  Key C1XS Features: Key XSM Features:
D-CIXS

Detectors: 24 swept charge devices of 1 cm2 each
Energy range: 1 – 10 keV
Spectral resolution: <110 eV @ 6.4 keV (pre-launch calibration)
Ground Pixel: 25 km × 25 km FWHM
Mass: 5.7 kg
Power supply: 35 – 42 V
In-flight calibration: door mounted X-ray sources
Filters: Al filters used to block sunlight
Elemental Range: Mg, Al, Si, Ca (Ti, Fe)

 

XSM Detector: Si-PIN
Energy range: 1 – 20 keV
Spectral resolution: ~200 eV @ 6 keV (pre-launch calibration)
FOV: 105°

X-ray Solar Monitor. IMAGE:  RAL

The X-ray solar monitor Example of one of C1XS's swept charge devices. Four of these will be mounted onto a ceramic strip to form a single SCD module.

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