Lander Specifications: Chandrayaan 3 Mission
Supporting Claims
The Lander for the Chandrayaan 3 mission is designed to function for the duration of one lunar day, equivalent to approximately 14 Earth days. With a combined mass of 1749.86 kg, including the Rover, it embodies a powerful setup, capable of generating 738 W of energy during the Winter solstice. The Lander's dimensions stand at 2000 x 2000 x 1166 mm, emphasizing its substantial build. It is geared for precise landing at a specified site, enhancing communication through ISDN, Ch-2 Orbiter, and the Rover. These specifications highlight the Lander's robustness and adaptability, essential for a successful lunar mission.
Rover Specifications: Chandrayaan 3 Mission
Supporting Claims
In the ambitious Chandrayaan 3 mission, the Rover stands as a technological marvel, designed to endure the lunar environment for the span of one lunar day, equivalent to approximately 14 Earth days. Its compact yet robust structure, weighing 26 kg, embodies adaptability and efficiency. Powered by a 50W system, the Rover is ready to navigate and execute its mission objectives with precision. Carrying a payload capacity of 2, it integrates crucial instruments and scientific tools. The Rover's physical dimensions, measuring 917 mm in length, 750 mm in width, and 397 mm in height, optimize its functionality on the lunar surface. Communication with the Lander establishes a vital link in this lunar exploration venture, enabling seamless coordination and data exchange.
Comprehensive Payload Overview for Chandrayaan 3 Mission
In the upcoming Chandrayaan 3 mission, a diverse range of payloads has been meticulously selected to unravel the mysteries of the lunar surface. Starting with the Lander's payloads, the RAMBHA-LP plays a crucial role by measuring near-surface plasma density, encompassing ions and electrons, and monitoring changes over time. Complementing this, ChaSTE, the Chandra's Surface Thermo-physical Experiment, will study thermal properties in the lunar surface's polar regions. Additionally, ILSA, the Instrument for Lunar Seismic Activity, aims to map seismicity around the landing site and decipher the lunar crust and mantle's structure.
Transitioning to the Rover, it houses the APXS (Alpha Particle X-Ray Spectrometer) to analyze chemical and mineralogical compositions, offering valuable insights into the lunar surface. The LIBS (Laser-Induced Breakdown Spectroscope) payload enables the determination of elemental composition in lunar soil and rocks, covering vital elements such as Mg, Al, Si, K, Ca, and Fe.
Lastly, the Propulsion Module Payload encompasses SHAPE, Spectro-polarimetry of HAbitable Planet Earth. This experimental payload seeks to study the spectro-polarimetric signatures of our habitable planet Earth, focusing on the near-infrared wavelength range (1-1.7 um). Together, these payloads contribute significantly to advancing our understanding of the Moon's composition, structure, and potential habitable environments.