ISRO's Semi-Cryogenic Engine Testing
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Questions and Answers

What is the propellant combination used in the semi-cryogenic engine being tested?

  • Liquid Nitrogen (LN) and Kerosene
  • Liquid Oxygen (LOX) and Hydrogen
  • Liquid Oxygen (LOX) and Kerosene (correct)
  • Liquid Nitrogen (LN) and Hydrogen

    • What is the purpose of the tests being conducted by ISRO?

  • 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

    • What is the thrust capability of the newly commissioned testing facility at IPRC?

  • Up to 3000 kN
  • Up to 2600 kN (correct)
  • Up to 4000 kN
  • Up to 2000 kN

    • What is the role of Liquid Propulsion Systems Centre (LPSC)?

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

    What were the chill-down operations carried out during the recent test at IPRC?

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

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