Mangalyaan was indian moon mission and which type of engines were used in the mission launch
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Propulsion: A liquid fuel engine with a thrust of 440 newtons (99 lbf) is usedfor orbit raising and insertion into Mars orbit. The orbiter also has eight 22-newton (4.9 lbf) thrusters for attitude control (orientation). Its propellant mass at launch was 852 kg (1,878 lb
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