Chandrayaan-1
http://www.mps.mpg.de/en/projekte/chandrayaan/index.html

Chandrayaan-1

India’s first scientific mission to Moon

> The Spacecraft
> The Launch
> Scientific objectives
> The payloads
> MPS contribution
> SIR-2

Spacecraft

Physical 1.5 m cuboid-shapped main body with a mass of about 600 kg in 100 km lunar orbit
Control 3-axis stabilized using reaction wheels and attitude control thrusters; sun sensors, star sensors, and miniaturized DTGs for orientation reference
Power Single sided solar array to generate 700 W, 36 Ah Li-Ion Battery for eclipse operations
Propulsion Bi-propellant system for transferring from initial(Earth) Orbit to Lunar Orbit and orientation maintenance
Communication TTC in S-band and scientific payload data transmission in X-band

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The Launch

Chandrayaan-1 was carried by Polar Satellite Launch Vehicle (PSLV-C11) from the second launch pad at Satish Dhawan Space Centre (SHAR), Sriharikota. Sriharikota is located in Andhrapardesh, the centre is 80 km north of Chennai in South India. The space craft was first placed into 250 km x 23000 km initial (Earth) orbit. Multiple perigee maneuvers carried out to achieve 380,000 km apogee [Lunar Transfer Trajectory (LTT)] in 17 days in Earth Bound Orbits prior to Lunar encounter. The space craft was successfully inserted into 100 km circular polar lunar orbit on 8 November 2008.

The Mission was declared over on 29 August 2009 after it stopped sending radio signals.

Lift-off of PSLV-C11 carrying Chandrayaan-1 Chandrayaan-1 mission profile
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Scientific objectives

The Chandrayaan-1 mission was aimed at high-resolution remote sensing of the Moon in visible, near Infrared, low energy X-ray and high-energy X-ray regions. Specifically, the objectives are:

The simultaneous photo-geological, mineralogical and chemical mapping through Chandrayaan-1 mission will enable identification of different geological units to infer the early evolutionary history of the Moon. The chemical mapping will enable to determine the stratigraphy and nature of the Moon’s crust and thereby test certain aspects of magma ocean hypothesis. This may allow to determine the compositions of impactors that bombarded the Moon during its early evolution, which is also relevant to the formation of the Earth.

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The payloads

Chandrayaan-1 had ten scientific payloads and an impact probe onboard.

Below is the summary of the prime objectives of the eleven payloads carried onboard Chandrayaan-1 mission.

Prime Objectives Payload
Chemical Mapping Chandrayaan-1 Imaging X-ray Spectrometer (C1XS) High Energy X-ray Spectrometer (HEX)
Mineralogical Mapping Hyper Spectral Imager (HySI) , Spectrometer InfraRed-2 (SIR-2) , Moon Mineralogy Mapper (M3)
Topography Mapping LLRI (Lunar Laser Ranging Instrument),TMC (Terrain Mapping Camera)
Radiation Environment Radiation Dose Monitor (RADOM), HEX, C1XS
Magnetic Field Mapping Sub KeV Atom Reflecting Analyser (SARA)
Volatile Transport HEX
Radio Mapping Miniature Synthetic Aperture Radar (Mini-SAR)
Lunar Atmospheric constituent MIP (Moon Impact Probe)


Summary of Chandrayaan-1 Prime Science Objectives and Wavelength Range Coverage
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MPS contribution

>SIR-2

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© 2009, Max-Planck-Institut für
Sonnensystemforschung, Lindau
Urs Mall
18-10-2009