pros:

• key components already flight proven (Draco, PICA-X, pressure shell, GN&C, water/parachute landing)
• full vertical integration of the whole stack in the same company
• redundant landing options (powered vs. parachute)
• reusable
• significantly lower retrieval cost (in powered landing)
• classic (proven) capsule design
• lowest cost per mission (estimated up to 140 million)

cons:

• toxic hypergolics used
• powered landing reduces usable mass to orbit
• powered landing not proven