PSLV-4

Stage · India

Original archive entry. The text, images and links below are kept as they were written.

ISRO N2O4/MMH rocket stage. Used on PSLV launch vehicle. First flight 1993.

Chamber Pressure: 8.40 bar. Area Ratio: 60. Thrust to Weight Ratio: 0. Coefficient of Thrust vacuum: 1.75.

No Engines: 2.

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