ISRO's Semi-Cryogenic Engine Testing

Liquid Nitrogen (LN) and Kerosene

Liquid Oxygen (LOX) and Hydrogen

Liquid Oxygen (LOX) and Kerosene (correct)

Liquid Nitrogen (LN) and Hydrogen

To build a state-of-the-art facility for space exploration

To assess the performance of existing launch vehicles

To develop and evaluate semi-cryogenic engines for future launch vehicles (correct)

To test fully integrated engines and stages

Up to 3000 kN

Up to 2600 kN (correct)

Up to 4000 kN

Up to 2000 kN

<p>Design and development of the semi-cryogenic engine</p> Signup and view all the answers

<p>Preparing the LOX circuit for engine start</p> Signup and view all the answers