Английская Википедия:ISRO Pad Abort Test

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Шаблон:Use dmy dates Шаблон:Use Indian English Шаблон:Infobox spaceflight

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.[1]

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.[2]

Flight

Файл:TVD1-Brochure elements 22.png
Launch Escape System
Файл:The Crew Module, part the Crew Escape System (CES), floating back to earth under its parachutes over the Bay of Bengal about 2.9 km from the Satish Dhawan Space Centre, Sriharikota.JPG
The Gaganyaan Crew Module boilerplate, after jettisoning the Crew Escape System (CES), floats back to the ground under its parachutes over the Bay of Bengal, about 2.9 km from the Satish Dhawan Space Centre, Sriharikota.

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[3] and reached a highest altitude of Шаблон:Convert, it later safely parachuted down and floated in the Bay of Bengal Шаблон:Convert 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.[4][5] Main objectives of test were nominal 20 second ascent and 200 seconds of descent, not including the splashdown.[6] Chute detachment was a scheduled event occurring around 259.4 seconds after launch as intended.[7][8]

Sequence of flight events.[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.

See also

References

Шаблон:Reflist

External links