Solar Depolyment Test Of Megha-Tropiques - Credit: ISRO
Description:
The french-indian Megha-Tropiques satellite is devoted to the atmospheric research. The data collected by the satellite will allow to
improve our knowledge on the water cycle contribution to the climate dynamic in the tropical atmosphere and our understanding of the processes
linked to the tropical convection.
MEGHA-TROPIQUES is a climate research mission to track tropical cyclones, monsoons and storm systems for at least three years.
Embarking on an international research mission, Megha-Tropiques has four instruments designed to probe the structure of the
atmosphere, measure temperature and water vapor, and study the Earth's radiation budget. India built the spacecraft, provided the
launch and contributed to two instruments. France supplied the satellite's water vapor profiling sensor and the radiation detector.
The satellite orbits about 538 miles (866 km) above Earth, crisscrossing the equator to cover an area stretching between 20
degrees north and south latitude.
The data collected by the satellite will allow improvement in knowledge on the water cycle contribution to the climate dynamic in the
tropical atmosphere and our understanding of the processes linked to the tropical convection.
Mission details:
India launched PSLV-C18, a PSLV-CA core-alone variant, from Sriharikota on Oct 12. The main payload of PSLV-C18 is the
Megha-Tropiques satellite, a joint Indian-French remote sensing satellite with a mass of around 1000 kg and based on the IRS
bus. It carries the MADRAS microwave imager, the Saphir water vapor profile instrument, and the ScaRaB radiation budget sanner.
Also carried were three small satellites: SRMSAT, from SRM University in Chennai, is a 10 kg satellite for greenhouse gas
monitoring. Jugnu, from the Indian Inst. of Technology in Kanpur is a 3U cubesat-class technology satellite.
VesselSat is a 29 kg small satellite built by OHB LuxSpace of Luxembourg to provide AIS (ship tracking) services for Orbcomm.
The five objects are in orbits with an apogee of 867 km and perigees ranging from 780 to 850 km; the low perigee object is
probably the rocket stage.