ISRO Conducts Full Nozzle Cryogenic Engine (CE-20) Test Outside Vacuum Chamber To Prepare For Inflight Re-Ignition

This test was done with multi element ignitor and water injection system at nozzle divergent to prevent flow separationISRO has successfully carried out the sea level hot test of its CE20 Cryogenic Engine featuring a nozzle area ratio of 100 at ISRO Propulsion Complex, Mahendragiri, Tamil Nadu on November 29, 2024. Performance of a multi-element igniter that is required for engine restart
This test was done with multi element ignitor and water injection system at nozzle divergent to prevent flow separationISRO has successfully carried out the sea level hot test of its CE20 Cryogenic Engine featuring a nozzle area ratio of 100 at ISRO Propulsion Complex, Mahendragiri, Tamil Nadu on November 29, 2024. Performance of a multi-element igniter that is required for engine restart
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