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Rocket Propulsion Analysis by K. Ramamurthi by Mohd Tauqeer is a document available to read on EtoBox.

What is Rocket Propulsion Analysis by K. Ramamurthi about?

The document discusses rocket propulsion and performance prediction analysis. It covers several key points: 1) It discusses different types of propellants that can be used in rockets, including liquid hydrogen/oxygen, hydrazine/N2O4, kerosene/oxygen, and solid fuel combinations like nitrocellulose and ammonium perchlorate with aluminum. 2) It describes how initial temperature and pressure of the propellants influences the combustion temperature and products. Higher pressure leads to less dissociation and

Author

Mohd Tauqeer

Language

EN