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A Crew Module Recovery Model (CMRM) that simulates the mass, center of gravity, outer dimensions, and externals of the actual Crew Module at touchdown was used for the trials at WSTF of Navy at Kochi in Kerala, the space agency said. The trials were part of the preparation for crew module recovery operations for the Gaganyaan mission that will be carried out in Indian waters with the participation of Indian Government agencies, the overall recovery operations being led by Indian Navy.
The sequence of operations required for the recovery of the Crew Module were carried out as part of the trials. Gaganyaan project envisages demonstration of human spaceflight capability by launching crew of three members to an orbit of 400 km for a three-day mission and bring them back safely to earth, by landing in Indian sea waters, according to ISRO. ”As the safe recovery of the crew is the final step to be accomplished for any successful human spaceflight, it is of paramount importance and it has to be carried out with the minimum lapse of time”, an ISRO statement said.
”Hence the recovery procedures for various scenarios need to be extensively practiced by carrying out a large number of trials. The Standard Operating Procedures (SoP) for recovery of Crew and Crew Module need to be finalised. The recovery trials will be initially carried out in a closed pool followed by trials in a harbor and in the open sea”, it said. The operations carried out on Tuesday form the initial recovery trials of Crew Module in a closed pool. Different phases of recovery trials starting with the recovery of the Crew Module to the flight crew training are planned at WSTF. WSTF is a state-of-the-art facility of the Indian Navy that provides realistic training of aircrew for escape from a ditched aircraft under varied simulated conditions and crash scenarios, the statement said. WSTF simulates different sea state conditions, environmental conditions, and day/night conditions. These trials assist in validating the SoP, and training recovery teams as well as the flight crew. They provide valuable inputs for the utilisation of recovery accessories, ISRO said.
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The engine with a nominal thrust of 80 ton is powering the second stages of PSLV & GSLV, liquid strapons of GSLV and the core liquid stage of LVM3. Liquid engines that support throttling of the engine thrust facilitate booster stage recovery in launch vehicles. Throttling of the engine was achieved by a closed loop thrust regulation system and the engine had been successfully throttled from the chamber pressure of 58.5 bar in steps of 50 bar, 45 bar & 40 bar, with dwelling at each pressure level for seven seconds. In addition, the Vikas engine was also throttled down to 45 per cent for the last three seconds before the engine shut down.
The results of the first hot test of Throttleable Vikas Engine on January 30 indicate stable combustion and subsystem performed in accordance with the prediction, ISRO said. The overall performance of engine sub-systems, control systems & test facility systems were as expected, it added.