Context: The Indian Space Research Organisation (ISRO) recently said that it has successfully developed a lightweight Carbon-Carbon (C-C) nozzle for rocket engines.
C-C nozzle
o Anti-Oxidation Coating: The nozzle boasts an anti-oxidation coating of Silicon Carbide, significantly expanding its operational capabilities in oxidizing environments.
o Enhanced Durability: This coating minimizes thermally induced stresses and enhances corrosion resistance, allowing for extended operational temperature limits in challenging environments.
o Potential Application in PSLV-4: The Polar Satellite Launch Vehicle (PSLV)-4 currently employs twin engines with nozzles made from Columbium alloy.
o Mass Reduction Potential: By substituting these engines with the C-C nozzle, a substantial mass reduction of approximately 67% can be achieved.
o Increased Payload Capability: This substitution is estimated to increase the payload capability of the PSLV by 15 kg, enhancing its efficiency and versatility.