Background

Chandrayaan-2 is India's second lunar mission, launched by ISRO in July 2019. While the Vikram lander lost communication during its landing attempt, the orbiter continues to provide valuable scientific data.

DFSAR Payload

The Dual Frequency Synthetic Aperture Radar (DFSAR) onboard Chandrayaan-2 orbiter is:

  • A microwave imaging instrument operating in L-band and S-band frequencies
  • First fully polarimetric synthetic aperture radar designed specifically to study the Moon

Key Findings

Study Focus

  • Targeted doubly shadowed craters located inside permanently shadowed regions
  • These regions experience extremely cold conditions of approximately 25 Kelvin (-248°C)
  • Such cold temperatures favour long-term preservation of water ice

Detection Details

  • Radar signatures indicated possible subsurface ice beneath four doubly shadowed craters
  • Strongest evidence from a 1.1 km-wide crater inside Faustini crater

Radar Criteria for Ice Detection

  • Circular Polarization Ratio (CPR) > 1
  • Degree of Polarization (DOP) < 0.13
  • These values indicate volumetric scattering associated with subsurface ice

Morphological Evidence

  • The crater inside Faustini showed lobate-rim morphology
  • Suggests that the impact event may have penetrated subsurface ice

Significance

  • Future Lunar Exploration: May help identify potential ice-bearing sites for landing missions
  • In-Situ Resource Utilisation (ISRU): Water ice can be used as a resource for future human missions
  • Scientific Understanding: Enhances knowledge of lunar volatiles and their distribution

Institutions Involved

  • Physical Research Laboratory (PRL), Ahmedabad - conducted the study
  • ISRO - provided the Chandrayaan-2 mission platform

Related Information

Chandrayaan-3 was India's subsequent lunar mission, continuing India's lunar exploration programme.