Based on propellant used in rockets , We can classify the rocket propulsion into following categories.
1.Solid Propellant Rocket
2.Liquid Propellant Rockets
3.Hybrid Rockets ( solid+liquid )
Rockets propulsion works with fuel ignition. And gets thrust by expelling mass at high speeds . For this we need propellant( fuel and oxidizer). In liquid propulsion we store oxidizer and fuel in different tanks . But this is not a case with Solid Rockets. Obviously ,we can get good combustion efficiency when the fuel and oxidizer are mixed properly. We can mix liquids easily , but it is not for solid rockets .
For this reason, we have to mix oxidizer and fuel. And should cast the propellant into Grains. Grains are cross-sectional structures of solid propellants . Maintaining grain shapes result in thrust characteristics with time. Different structure shows different results. So we have to select the grain structure based on our requirements. Having space in center of grains creates more efficiency rather than completely gets filled with propellant.
The below are few widely propellants in missions.
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