# ISRO Pad Abort Test

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Indian Space Research Organization launch test

ISRO Pad Abort Test 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 IHSP ← CARE TV-D1 →

The **ISRO Pad Abort Test** was a [launch escape system](/source/Launch_escape_system) test by [ISRO](/source/ISRO) of its crew module as part of [Indian Human Spaceflight Programme](/source/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](/source/Gaganyaan)*, scheduled to be launched no earlier than 2024.[3]

## Flight

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](/source/Bay_of_Bengal), about 2.9 km from the [Satish Dhawan Space Centre](/source/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](/source/Satish_Dhawan_Space_Centre). The crew module was accelerated to 10 [g](/source/G-force)[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](/source/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]

Sequence of flight events.[10] 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

- [Gaganyaan](/source/Gaganyaan), India's crewed spacecraft

- [Indian Human Spaceflight Programme](/source/Indian_Human_Spaceflight_Programme)

- [Launch escape system](/source/Launch_escape_system)

## References

1. **[^](#cite_ref-Rajyasabha_1-0)** ["Parliamentary Q&A \[25 Nov 2016\]: Queries on Crew Escape System, Chandrayaan-2 rover and MOM-2"](https://www.reddit.com/r/ISRO/comments/5et61z/parliamentary_qa_25_nov_2016_queries_on_crew). 25 November 2016.

1. **[^](#cite_ref-2)** ["ISRO conducts pad abort test for Indian human space flight program – NASASpaceFlight.com"](https://www.nasaspaceflight.com/2018/07/isro-pad-abort-test-indian-human-program/). *www.nasaspaceflight.com*. 4 July 2018. Retrieved 5 July 2018.

1. **[^](#cite_ref-3)** ["Gaganyaan mission can't happen this year or next year, focus fully on safety aspects: Isro chief"](https://timesofindia.indiatimes.com/india/gaganyaan-mission-cant-happen-this-year-or-next-year-focus-fully-on-safety-aspects-isro-chief/articleshow/92579979.cms). *The Times of India*. 30 June 2022. [ISSN](/source/ISSN_(identifier)) [0971-8257](https://search.worldcat.org/issn/0971-8257). Retrieved 21 May 2023.

1. **[^](#cite_ref-4)** Baluragi, Hanamantray; Suresh, Byrana Nagappa (2020), ["Indian Space Program: Evolution, Dimensions, and Initiatives"](http://link.springer.com/10.1007/978-3-030-22786-9_38-2), *Handbook of Space Security*, Cham: Springer International Publishing, pp. 1–19, [doi](/source/Doi_(identifier)):[10.1007/978-3-030-22786-9_38-2](https://doi.org/10.1007%2F978-3-030-22786-9_38-2), [ISBN](/source/ISBN_(identifier)) [978-3-030-22786-9](https://en.wikipedia.org/wiki/Special:BookSources/978-3-030-22786-9), [S2CID](/source/S2CID_(identifier)) [216447640](https://api.semanticscholar.org/CorpusID:216447640), retrieved 4 July 2020{{[citation](https://en.wikipedia.org/wiki/Template:Citation)}}: CS1 maint: work parameter with ISBN ([link](https://en.wikipedia.org/wiki/Category:CS1_maint:_work_parameter_with_ISBN))

1. **[^](#cite_ref-thehindu_5-0)** ["ISRO's first 'pad abort' test, critical for future human space mission, successful"](https://www.thehindu.com/sci-tech/technology/isros-first-pad-abort-test-successful/article24336860.ece).

1. **[^](#cite_ref-6)** ["SUCCESSFUL FLIGHT TESTING OF CREW ESCAPE SYSTEM - TECHNOLOGY DEMONSTRATOR - ISRO"](https://web.archive.org/web/20180705234350/https://www.isro.gov.in/hi/update/05-jul-2018/successful-flight-testing-of-crew-escape-system-technology-demonstrator). *www.isro.gov.in*. Archived from [the original](https://www.isro.gov.in/hi/update/05-jul-2018/successful-flight-testing-of-crew-escape-system-technology-demonstrator) on 5 July 2018. Retrieved 5 July 2018.

1. **[^](#cite_ref-7)** ["ISRO's Human Space Programme: Pad Abort Test (PAT) on 5th July, 2018 Early Morning"](https://web.archive.org/web/20180704173738/http://www.sac.gov.in/SacSliderI_Repository/Vyom/English/585/SSAA_HSP-PAT-CES-FLASH_2July2018.pdf) (PDF). 4 July 2018. Archived from [the original](http://www.sac.gov.in/SacSliderI_Repository/Vyom/English/585/SSAA_HSP-PAT-CES-FLASH_2July2018.pdf) (PDF) on 4 July 2018.

1. **[^](#cite_ref-8)** ["Episode 80 - S Somnath Director of Vikram Sarabhai Space Centre"](https://astrotalkuk.org/episode-80-s-somnat-director-of-vikram-sarabhai-space-centre/). *AstrotalkUK*. 30 November 2018. Retrieved 12 January 2020.

1. **[^](#cite_ref-9)** ["Flight test of crew escape system - Technology Demonstrator Lift of video - ISRO"](https://web.archive.org/web/20210226071754/https://www.isro.gov.in/flight-test-of-crew-escape-system-technology-demonstrator-lift-of-video). *www.isro.gov.in*. Archived from [the original](https://www.isro.gov.in/flight-test-of-crew-escape-system-technology-demonstrator-lift-of-video) on 26 February 2021. Retrieved 12 January 2020.

1. **[^](#cite_ref-10)** Kunhikrishnan, P. (15 February 2019). ["Recent Indian Space Missions: Update as of February 2019"](http://www.unoosa.org/documents/pdf/copuos/stsc/2019/tech-25E.pdf) (PDF).

## External links

- [Official video](https://www.isro.gov.in/flight-test-of-crew-escape-system-technology-demonstrator-lift-of-video) [Archived](https://web.archive.org/web/20210226071754/https://www.isro.gov.in/flight-test-of-crew-escape-system-technology-demonstrator-lift-of-video) 26 February 2021 at the [Wayback Machine](/source/Wayback_Machine)

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Adapted from the Wikipedia article [ISRO Pad Abort Test](https://en.wikipedia.org/wiki/ISRO_Pad_Abort_Test) by Wikipedia contributors ([contributor history](https://en.wikipedia.org/wiki/ISRO_Pad_Abort_Test?action=history)). Available under [Creative Commons Attribution-ShareAlike 4.0 International](https://creativecommons.org/licenses/by-sa/4.0/). Changes may have been made.
