At the same time, engineering and operational constraints are needed to ensure the safe entry, descent and landing of the entry module. These include a relatively low-lying site, in order that the module passes through enough atmosphere for the completion of key events such as parachute opening and deceleration. The horizontal and vertical wind speeds expected during the descent must also be also considered.
Knowledge of how the terrain slopes over various scales is important, because the lander uses radar to monitor its velocity and altitude. Slopes can alter the degree of certainty in the measured distance to the ground, with implications for fuel consumption and landing. Steep slopes and boulders taller than 35 cm – the clearance beneath the landing module – need to be avoided, although the rover will be able to navigate around local hazards after egress.