Formal MoU was signed on Feb 26, 2020. The collaboration was initiated through discussions happened during the third edition of Bonjour India organised by French Embassy in India at Bangalore on 29th and 30th January 2018. The major collaborative research projects carried out/in progress are the following.
A cubesat constellation mission for multipoint measurements on mars: Completed
The project was to assess the feasibility of CubeSat technology for obtaining multipoint measurements around Mars. Due to the complex interactions between the Martian atmosphere, magnetosphere, and its surface, multipoint simultaneous measurements will pave way for understanding of the dynamics and origins of Mars’ current state in a new way. This Indo-French collaborative study focuses on using existing as well as developing CubeSat technologies from India and France for the scientific mission.
Piggy-back Launch for Deep Space Exploration-2019: Completed
This project assesses this feasibility with trajectories towards NEOs and Mars, the nearest objects of Earth. The package pykep implemented by ESA on Python, gives a first good estimation of potential optimal low-thrust trajectories with mass required for the travel. Simulations reveal this solution is possible for deep space exploration with small satellites launched on a GTO or with a dedicated launch, using electric propulsion.
Comet Sample return, mission concepts from an Indo-French team: Completed
The main objective of the proposal was to conceptualize, design and simulate a sample return mission form a comet in the year 2035 to 2045 time frame using the capabilities of Arian 6 to GSLV Mk. III launcher. Two of the most crucial and unprecedented components of the mission were obtain a cometary sample from at least 50 cm below the surface while marinating the stratigraphy and to bring the samples back to earth while maintaining cryogenic temperatures. Both the aspects were extremely challenging and being attempted for the first time.
A mission to probe upper atmosphere of Venus and its interaction with solar winds using adaptable 1 + 8 satellite formation : Proposal approved, work started from October 2021 onwards
The project proposed here is to explore Venus, one of our nearest neighboring planets. The main goal of the mission would be to design a single mother ship and eight daughter nano satellites configuration flying at three altitudes in 4S top + 1M + 4S bottom configuration and probe compositional variation in real time. The investigation can target not only the atmospheric composition but also the interaction of solar wind in the upper atmosphere of Venus. Altitudes above 150 km will be very interesting.