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Solid Propellant Design for SLWS by Marcos Florez is a document available to read on EtoBox.

What is Solid Propellant Design for SLWS about?

This document discusses specific design features of solid propellant rocket motors used in shoulder-launched weapon systems. It analyzes published data on four short-burning rocket motors: the gas generator and correction impulse rocket motors from the Dragon missile system, the 68mm Zolja rocket motor, and the 90mm OSA rocket motor. The document notes that rocket motors for shoulder-launched weapons have extremely short burn times measured in milliseconds, very high chamber pressures, and require reliable

Author

Marcos Florez

Language

EN