Design and analyze a multi$-$stage rocket propulsion system for interplanetary missions. Given:Specify the payload capacity, mission duration, and target destination within the solar system.Design propulsion stages using liquid and solid rocket engines for launch, orbit insertion, and interplanetary transfer.Evaluate the thrust$-$to$-$weight ratio, specific impulse, and propellant mass fractions for each stage to optimize fuel efficiency and payload capacity.Discuss the integration of navigation systems, trajectory planning algorithms, and orbital mechanics simulations for accurate mission planning.Analyze thermal management strategies, including heat shield design and active cooling systems, to withstand re$-$entry and extreme space conditions.Propose reliability engineering measures such as redundancy in avionics, telemetry systems, and fault detection algorithms for mission success in deep space.Assess environmental sustainability considerations, including space debris mitigation and orbital decay management during mission operations.

What is DBMS$?$