the 8 0 0 kg wet mass mars polar lander consumes 2 5 0 kgs of fuel
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the kg wet mass mars polar lander consumes kgs of fuel to reach a circular polar low mars orbit of km from mars surface. ML makes a powered landing from a m altitude. calculate the minimum DV time and fuel with an average Ispg of ms required to reach mars surface. neglect fuel required to lanlands from the km altitude. what may be the thrust level of onboard thrusters to land the lander if it has equal thursters? please make a sketch and state your assumptions for each step.
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