It has a total nominal mass of 6001 kg, of which 5444 kg is propellant load and its burn out mass is 529 kg. It has an average thrust of 190 kN with a specific impulse of 292 seconds burning for 87 seconds, with a total impulse of 1.589 MN. It is spin stabilized at 40 rpm and the propellant mass can be reduced by up to 350 kg eight months before launch or up to 15 kg on the launch site.

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