0.5.12 - ci-build
SpaceflightHealthSimulationsReferenceDocumentation - Local Development build (v0.5.12) built by the FHIR (HL7® FHIR® Standard) Build Tools. See the Directory of published versions
| Official URL: http://hl7.org/fhir/uv/aerospace/ValueSet/crewed-mars-missions-vs | Version: 0.5.12 | |||
| Active as of 2026-03-25 | Computable Name: CrewedMarsMissionsVS | |||
Proposed and conceptual human mission architectures to Mars
References
This value set is not used here; it may be used elsewhere (e.g. specifications and/or implementations that use this content)
http://hl7.org/fhir/uv/aerospace/CodeSystem/crewed-mars-missions-cs version 📦0.5.12
Expansion performed internally based on codesystem Human Mars Mission Plans v0.5.12 (CodeSystem)
This value set contains 10 concepts
| System | Code | Display (en) | Definition | JSON | XML |
http://hl7.org/fhir/uv/aerospace/CodeSystem/crewed-mars-missions-cs | marsDirect | Mars Direct (Zubrin 1990) | Two-launch architecture with ISRU propellant production on Mars, direct Earth-Mars transit, 18-month surface stay, artificial gravity tether, crew of 4 | ||
http://hl7.org/fhir/uv/aerospace/CodeSystem/crewed-mars-missions-cs | nasaDRM1 | NASA Design Reference Mission 1.0 (1993) | NASA's first Mars Semi-Direct adaptation, split missions with ISRU but added Mars Orbit Rendezvous with MAV | ||
http://hl7.org/fhir/uv/aerospace/CodeSystem/crewed-mars-missions-cs | nasaDRM3 | NASA Design Reference Mission 3.0 (1998) | NASA DRM evolution with increased crew size (6) and hardware redundancy, Semi-Direct architecture | ||
http://hl7.org/fhir/uv/aerospace/CodeSystem/crewed-mars-missions-cs | nasaDRA5 | NASA Design Reference Architecture 5.0 (2009) | Conjunction-class mission with ~3 launches, nuclear thermal rockets for cargo, fission surface power (~25 kW), long surface stays | ||
http://hl7.org/fhir/uv/aerospace/CodeSystem/crewed-mars-missions-cs | austereMars | NASA Austere Human Missions to Mars (2009) | Cost-reduced DRA 5.0 variant with simplified technology, 4 crew, reduced infrastructure | ||
http://hl7.org/fhir/uv/aerospace/CodeSystem/crewed-mars-missions-cs | journeyToMars | NASA Journey to Mars (2015) | Moon-first strategy (Artemis), then Mars in 2030s, incremental capability buildup, Gateway staging | ||
http://hl7.org/fhir/uv/aerospace/CodeSystem/crewed-mars-missions-cs | spacexStarship | SpaceX Starship Mars Plan (2016-present) | Commercial plan using fully reusable Starship, orbital refueling (10-14 tankers), ISRU for return, target ~2029-2031 | ||
http://hl7.org/fhir/uv/aerospace/CodeSystem/crewed-mars-missions-cs | marsOne | Mars One (2012-2019) | Private one-way colonization concept, planned 2023 launch, project defunct 2019 | ||
http://hl7.org/fhir/uv/aerospace/CodeSystem/crewed-mars-missions-cs | inspirationMars | Inspiration Mars (2013) | Proposed crewed Mars flyby (Dennis Tito plan for 2018 launch window), not surface landing | ||
http://hl7.org/fhir/uv/aerospace/CodeSystem/crewed-mars-missions-cs | projectOlympus | Project Olympus / Athena (2025) | Jared Isaacman plan for accelerated NASA-commercial Mars efforts, uncrewed demo by 2026, nuclear-electric propulsion priority |
Explanation of the columns that may appear on this page:
| Level | A few code lists that FHIR defines are hierarchical - each code is assigned a level. In this scheme, some codes are under other codes, and imply that the code they are under also applies |
| System | The source of the definition of the code (when the value set draws in codes defined elsewhere) |
| Code | The code (used as the code in the resource instance) |
| Display | The display (used in the display element of a Coding). If there is no display, implementers should not simply display the code, but map the concept into their application |
| Definition | An explanation of the meaning of the concept |
| Comments | Additional notes about how to use the code |