ISRO (Indian Space Research Organisation) has successfully developed a cost-effective, single-stage test vehicle powered by the Vikas engine. This vehicle will be used to validate the Crew Escape System (CES), a critical safety feature for astronaut missions.
The Crew Escape System is a vital emergency safety mechanism designed to protect astronauts in the event of a launch abort. In such an emergency, the system quickly pulls the crew module (which houses the astronauts) to a safe distance from the launch vehicle to prevent potential harm.
CES can be classified into two types, based on the method of extracting the crew module:
Puller Type CES:
Used in India's Gaganyaan mission.
The CES pulls the crew module away from the failing launch vehicle.
This system uses solid or liquid fuel rockets to separate the crew capsule from the rocket.
Pusher Type CES:
Used in vehicles like SpaceX's Falcon 9.
The crew module is pushed away from the launch vehicle using high-thrust liquid-fuel engines.
Notable examples of the Puller Type CES include NASA’s Saturn V, Russia’s Soyuz, and China’s Long March rockets.
Activation of CES:
The CES is activated automatically when an anomaly or emergency is detected. The Integrated Vehicle Health Management (IVHM) system plays a key role in this process.
The IVHM system is a network of sensors, electronics, and software that constantly monitors the vehicle’s and crew’s health during the mission. It tracks the vital parameters of both the vehicle’s systems and the astronauts.
The IVHM ensures early detection of issues, minimizes false alarms, and triggers the CES as soon as a safety risk is identified.
Escape Procedure:
Once the CES is activated, the crew module is pulled to a safe distance from the launch vehicle.
After separation, the crew module undergoes a controlled deceleration using a multistage parachute system. This slows the module down in steps to ensure a safe splashdown.
The parachute system ensures that the crew does not experience excessive forces, reducing the risk of injury upon impact with the water.
Safe Landing:
The astronauts remain inside the module until it reaches the splashdown point.
The system’s precise control ensures the module lands safely in the ocean without exceeding the crew’s physiological limits.
Vikas Engine: A key component powering the single-stage test vehicle used for validating CES by ISRO. The Vikas engine is used in various ISRO missions and has been modified to suit the requirements of the CES.
Integrated Vehicle Health Management System (IVHM): A crucial safety system that continuously monitors the health of the spacecraft, detecting any anomalies and triggering the CES when needed. It ensures that real-time data from various vehicle systems and crew health parameters are analyzed and used to make critical decisions about when to activate the escape system.
The development and successful validation of CES represent a major milestone in India's space exploration capabilities, particularly for the Gaganyaan mission, which is ISRO's first manned mission to space.
By incorporating a cost-effective, single-stage test vehicle, ISRO is able to demonstrate the feasibility and reliability of this escape system, ensuring the safety of the astronauts during all stages of the mission.
The successful testing of CES is also a testament to India’s growing space technology prowess, positioning ISRO as a leader in human spaceflight alongside other space agencies such as NASA and the European Space Agency.
ISRO's development of the Crew Escape System (CES) is a significant step forward in ensuring the safety of astronauts during high-risk phases of space missions. With cost-effective design, advanced health monitoring systems, and reliable escape mechanisms, ISRO aims to minimize risks for astronauts, enhancing the success and safety of the Gaganyaan mission and future manned space flights.
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