Gelled propellants are improved propellants that can be considered as the final extension of liquid propellants. High specific impulse, good density, a safety better than that of both solid and liquid propellants and thrust management ability are some of the advantages of these propellants compared with common solid and liquid propellants. In early decades, an extensive research has been carried out on making, quality control, combustion and application of these propellants. Gelled propellants can be used in air breathing systems, pilot seat ejection systems, smart propulsion missiles, advanced launch-vehicle boosters, etc. In this research a review of the papers on making gelled propellants was carried out, on the basis of which, the basic properties and characteristics of gelled propellants are described. Then methods for making important gel fuels and oxidizers such as, hydrazine, mono methyl hydrazine (MMH), unsymmetrical dimethyl hydrazine (UDMH), kerosene, inhibited red fuming nitric acid (IRFNA) and nitrogen tetroxide are presented. Next gelled simulants, their applications and preparation methods as a background for making main gelled propellants are described. In order to study the possibility of making MC-UDMH gelled propellants, MC-H2O gelled simulant was made in the laboratory and the rheological behavior of this simulant was investigated. Results showed that the prepared MC-H2O gel has good rheological behavior and can be used as a simulant for UDMH gelled propellants.