Mission type | Launch escape system |
---|---|
Operator | ISRO |
Mission duration | 4 minutes, 25 seconds |
Apogee | 2.75 km (1.71 mi), |
Spacecraft properties | |
Spacecraft type | Gaganyaan's boilerplate vehicle |
Manufacturer | ISRO |
Launch mass | 12.6 ton [1] |
Start of mission | |
Launch date | 5 July 2018 |
Launch site | Satish Dhawan Space Centre |
The ISRO Pad Abort Test was an Indian Space Research Organisation launch escape system test of its crew module as part of Indian Human Spaceflight Programme. The successful test took place on 5 July 2018. [2]
A Pad Abort Test is a trial run for the spacecraft's launch abort system (sometimes called a launch escape system). This system is designed to quickly get the crew and spacecraft away from the rocket in the event of a potential failure. It is similar to an ejection seat for a fighter pilot, but instead of ejecting the pilot out of the spacecraft, the entire spacecraft is "ejected" away from the launch vehicle. The technology developed is expected to be applied to the first Indian crewed spacecraft called Gaganyaan , scheduled to be launched no earlier than 2024. [3]
The countdown for the test started at 2:00 am (IST) on 5 July 2018. At 7:00 am (IST) The Crew Escape System with crew module successfully lifted-off from Satish Dhawan Space Centre. The crew module was accelerated to 10 g [4] and reached a highest altitude of 2.75 km (1.71 mi), it later safely parachuted down and floated in the Bay of Bengal 2.9 km (1.80 mi) away from its launch site. It was carried skyward using seven solid-fueled rocket motors keeping within the safe g-force limits. Later recovery boats were sent to recover the crew module. The total duration of the test mission was 259 seconds. The test launch process was recorded by around 300 sensors. [5] [6] Main objectives of test were nominal 20 second ascent and 200 seconds of descent, not including the splashdown. [7] Chute detachment was a scheduled event occurring around 259.4 seconds after launch as intended. [8] [9]
Time | Event |
---|---|
T0 - 30 minutes | Grid fins deployed |
T0 - 8 seconds | Separation from launchpad |
T0 | Ignition of High Altitude Escape Motor (HEM) and Low Altitude Escape Motor (LEM) |
T0 + 0.9 seconds | Ignition of Pitch Motor (PM) |
T0 + 2 seconds | Burnout of Pitch Motor (PM) |
T0 + 5 seconds | Burnout of High Altitude Escape Motor (HEM) |
T0 + 8 seconds | Burnout of Low Altitude Escape Motor (LEM) |
T0 + 18 seconds | Crew Escape System/Crew Module aft link separation |
T0 + 20 seconds | Crew Escape System/Crew Module separation, jettisoning motor ignition |
T0 + 29 seconds | Parachute deployment |
T0 + 265 seconds | Crew Module Splashdown. |
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Human spaceflight programs have been conducted, started, or planned by multiple countries and companies. Until the 21st century, human spaceflight programs were sponsored exclusively by governments, through either the military or civilian space agencies. With the launch of the privately funded SpaceShipOne in 2004, a new category of human spaceflight programs – commercial human spaceflight – arrived. By the end of 2022, three countries and one private company (SpaceX) had successfully launched humans to Earth orbit, and two private companies had launched humans on a suborbital trajectory.
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A launch escape system (LES) or launch abort system (LAS) is a crew-safety system connected to a space capsule. It is used in the event of a critical emergency to quickly separate the capsule from its launch vehicle in case of an emergency requiring the abort of the launch, such as an impending explosion. The LES is typically controlled by a combination of automatic rocket failure detection, and a manual activation for the crew commander's use. The LES may be used while the launch vehicle is on the launch pad, or during its ascent. Such systems are usually of three types:
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