As the engineering team, we want a detailed design for the spacecraft's Service Module (SM) to ensure it supports the vehicle's operations throughout the Mars mission.
Acceptance Criteria
[ ] SM shall provide propulsion capability for Mars transfer, orbit insertion, and return journey.
[ ] SM shall house the life support systems necessary to sustain the crew for the duration of the mission.
[ ] SM shall be equipped with thermal control systems to maintain operational temperature ranges for all onboard systems and crew environment.
[ ] SM must support communication with Earth throughout the mission with minimum data transfer rate requirements.
[ ] SM should integrate seamlessly with the Crew Module (CM) and ensure crew safety in case of emergency separation.
[ ] SM shall have redundancy in critical systems such as life support, communication, and propulsion.
[ ] SM shall be equipped with solar panels capable of providing sufficient power for the entire mission duration.
graph LR
A[Service Module] -- Propulsion --> B[Mars Transfer]
A -- Life Support --> C[Crew Module]
A -- Thermal Control --> D[Environmental Regulation]
A -- Communication --> E[Earth]
A -- Solar Panels --> F[Power Generation]
A -- Redundancy --> G[Critical Systems]
Service Module Specifications
As the engineering team, we want a detailed design for the spacecraft's Service Module (SM) to ensure it supports the vehicle's operations throughout the Mars mission.
Acceptance Criteria