File:Uprated CE-20 engine E9 going through 70 second duration hot test at Cryo Main Engine and Stage Test Facility at IPRC, Mahendragiri on 9 Nov 2022 01.webp
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![File:Uprated CE-20 engine E9 going through 70 second duration hot test at Cryo Main Engine and Stage Test Facility at IPRC, Mahendragiri on 9 Nov 2022 01.webp](https://upload.wikimedia.org/wikipedia/commons/thumb/c/c0/Uprated_CE-20_engine_E9_going_through_70_second_duration_hot_test_at_Cryo_Main_Engine_and_Stage_Test_Facility_at_IPRC%2C_Mahendragiri_on_9_Nov_2022_01.webp/800px-Uprated_CE-20_engine_E9_going_through_70_second_duration_hot_test_at_Cryo_Main_Engine_and_Stage_Test_Facility_at_IPRC%2C_Mahendragiri_on_9_Nov_2022_01.webp.png?20221110142638)
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[edit]DescriptionUprated CE-20 engine E9 going through 70 second duration hot test at Cryo Main Engine and Stage Test Facility at IPRC, Mahendragiri on 9 Nov 2022 01.webp |
English: On 9 November 2022, CE-20 engine E9 was hot tested for 70 seconds. During this test the engine operated at thrust level of approximately 20 tonnes for the first 40 seconds and then switched to an uprated thrust regime of 21.8 tonnes lasting ~30 seconds. This uprated engine would increase payload capacity of LVM3 to GTO by up to 450 kg along an appropriate stage with additional propellant loading. |
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Source | https://www.isro.gov.in/LVM3_CE20_uprated_Engine_Hot_Test.html |
Author | Indian Space Research Organisation |
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This file is a copyrighted work of the Government of India, licensed under the Government Open Data License - India (GODL).
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Attribution: Indian Space Research Organisation (GODL-India) | ||
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current | 14:26, 10 November 2022 | ![]() | 1,024 × 682 (81 KB) | Ohsin (talk | contribs) | Uploaded a work by Indian Space Research Organisation from https://www.isro.gov.in/LVM3_CE20_uprated_Engine_Hot_Test.html with UploadWizard |
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