Fig. 6.

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How the environment removes gas from an example satellite. For an example gas-poor satellite today of mass in a cluster of mass
, we study the time evolution of the gas radial profiles since first infall (τFirstInfall ≈ 8.6 Gyr i.e., look-back time ≈5 Gyr) until it becomes gas-poor today. The cumulative environmental effects, namely the integrated ram pressure since infall, and secular processes, namely feedback from the SMBH, remove the satellite’s gas, leaving a gas-poor, quenched satellite today.
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