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Source: TH
Also Read > Pradhan Mantri Bharatiya Janaushadhi Kendras (PMBJK).
Also Read > Geological Survey of India
Bhaskaracharya National Institute for Space Applications and Geo-informatics (BISAG-N)
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| Feature | Cryogenic Engine | Semi-Cryogenic Engine |
| Propellant | LOX + Liquid Hydrogen (LH2) | LOX + Kerosene |
| Storage Temperature | -253°C (LH2) | LOX at -183°C, kerosene at room temperature |
| Thrust | High impulse, but lower density | Higher density impulse, greater thrust per volume |
| Handling Complexity | More complex; it requires extreme cooling | Easier storage and handling |
| Reusability | Lower due to fuel volatility | Higher due to simpler fuel management |

Credit: ABC News

Source: Peoples