Satellite launch vehicle technologies is an important field to explore as it brings tremendous advantages for the well establishment of our society, which can play a crucial role to boost nations economic business through Telecom technology, weather forecasts, military services, and scientific technologies explorations. So, hydrazine is well known as the fuel of the satellite vehicles, which is converted to (N2/H2) in the vehicle thrusters. Indeed, for the well travelling of the satellite vehicle from earth station to the space orbits, hydrazine is among the used fuels . For this hydrazine catalytic decomposition in the thruster of the satellite vehicle, a commercial shell 405 catalyst is used for better purposes. So, since the development of shell 405 catalyst, a considerable work have been established to master this chemical reaction technology. In the same way, in 2011, Soares Neto, T. G., et al prepared a Ir anchored on alumina support with only 30% of iridium charges, for monopropellant hydrazine decomposition in a 2 N satellite thruster technology. This particular study made an attention on catalysts textural evolution under the hydrazine decomposition reaction (HzDR). Another analysis reported by Jofre, J.B.F., et al described that both monometallic (Ir/Al2O3) and bimetallic (Ir-Ru/Al2O3) catalytic behaviour is similar to that of shell 405 commercial catalyst for hydrazine monopropellant decomposition reaction in the 5 N satellite thruster. However, the catalyst which does not contains iridium metal nanoparticles (Ru/Al2O3) shows lower catalytic performance for this particular reaction. And (Ru/Al2O3) catalyst shouldn't be advisable for uses in cold starts technology. This highlights that iridium materials and his related composites are interesting for this reaction. Vieira, R., et al demonstrated the use of carbon nanofibers as a support of the well known irridium for this chemical technology. In fact, the as prepared Ir/CNF catalyst reveal higher catalytic hydrazine decomposition performance than that of shell 405 catalyst under the studied conditions. The superior activity were attributed to the open structure of CNF with higher external surface area, and the lack of any closed porosity, which significantly boosted the contact between hydrazine and active sites. Also, the Ir/CNF catalyst exhibited strong catalytic stability. Moreover, the decomposition of hydrazine is described to goes in two ways, the indirect pathway, which produces ammonia and nitrogen at low temperature, the produced NH3 is further converted to (N2/H2), and the direct pathway, which yields (N2/H2) without any trace of NH3 as described in . The two pathways are shown below. Due the high cost, limited reserves, and as well as performances of noble metals for hydrazine decay related. The search of abundant earth metal materials with cost-effectiveness must be accelerated for affordable satellite thruster technologies. Therefore, in this research manuscript, it is focused on the recently developed molybdenum based catalysts for high performance hydrazine monopropellant Thrusters, for Satellites launch vehicle technologies. Also, it shows further catalytic applications of (Mo) based materials in interaction with hydrazine chemical fuel.