Millennium Post Siliguri

ISRO develops innovative, lightweigh­t nozzle for rocket engines

Substituti­ng metallic nozzles with carbon-carbon counterpar­ts reduces mass by 67%, increasing PSLV payload capability by 15 kg

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BENGALURU: ISRO said it has achieved a breakthrou­gh in rocket engine technology with the developmen­t of a lightweigh­t Carbon-Carbon (C-C) nozzle for rocket engines, enhancing payload capacity.

This innovation accomplish­ed by the space agency’s Vikram Sarabhai Space Centre (VSSC) promises to enhance the vital parameters of rocket engines, including thrust levels, specific impulse, and thrust-toweight ratios, thereby boosting the payload capacity of launch vehicles, it said. Thiruvanan­thapuram-based VSSC leveraged advanced materials like Carbon-Carbon (C-C) composites to create a nozzle divergent that offers exceptiona­l properties, an ISRO statement said. By utilising processes such as carbonisat­ion of green composites, chemical vapor Infiltrati­on, and high-temperatur­e treatment, it has produced a nozzle with low density, high specific strength, and excellent stiffness, capable of retaining mechanical properties even at elevated temperatur­es, it said.

A key feature of the C-C nozzle is its special anti-oxidation coating of silicon carbide, which extends its operationa­l limits in oxidising environmen­ts. This innovation not only reduces thermally induced stresses but also enhances corrosion resistance, allowing for extended operationa­l temperatur­e limits in hostile environmen­ts, according to ISRO.

The potential impact of this developmen­t is significan­t, particular­ly for the ISRO’s workhorse launcher, the Polar Satellite Launch Vehicle (PSLV). The PS4, the fourth stage of the PSLV, currently employs twin engines with nozzles made from columbium alloy. However, by replacing these metallic divergent nozzles with C-C counterpar­ts, a mass reduction of approximat­ely 67 per cent can be achieved, the space agency said.

This substituti­on is projected to increase the payload capability of the PSLV by 15 kg, a notable enhancemen­t for space missions. The successful testing of the C-C nozzle divergent marked a major milestone for ISRO.

 ?? ?? Carbon-carbon nozzle features anti-oxidation coating for extended operationa­l limits, reducing thermally induced stresses and enhancing corrosion resistance
Carbon-carbon nozzle features anti-oxidation coating for extended operationa­l limits, reducing thermally induced stresses and enhancing corrosion resistance

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