Glossary¶
Summary. ADD Rev C's Appendix F, "Terminology" (pp. 291–304), has three parts. F.1 lists 112 acronyms with a "Usage/Context" column, F.2 defines 107 terms, and F.3 sets the rough quantities behind words like "limited" and "moderate" in the objective decomposition. This page gives all three in NASA's wording. It then sets F's definitions beside the other places the architecture defines the same words: the ADD's own key-terms tables, its Appendix C, the 2025 "Architecture Definition" white paper, the 2022 objectives glossary and the 2023–2024 executive overviews. Most match. The real differences are "trade space", which Appendix F defines unlike everywhere else, and a few smaller shifts ("function", "exploration asset", "legacy decision", "continuous presence"). Appendix F predates the Moon Base and has no Moon Base terms. It doesn't define "technology gap" or "Mars vicinity" either.
All page numbers are ADD Rev C unless marked otherwise. The text layer splits several glossary rows from their terms, so pp. 291–294, 298 and 300–302 and p. 304 were checked against the PDF. The "Wiki pages" column and every comparison on this page are the wiki's, not NASA's.
Contents¶
- Acronyms (F.1)
- Terms (F.2)
- Quantity descriptors (F.3)
- Same word, other definitions
- What Appendix F leaves out
Appendix F's one-line introduction: "This appendix captures acronyms and abbreviations, defines terms used throughout the document" (p. 291, as printed).
Acronyms (F.1)¶
F.1, "Acronyms and Abbreviations" (pp. 291–294), in the printed order. The third column is NASA's "Usage/Context", left blank where the ADD leaves it blank.
| Acronym | Meaning | Usage/Context | Wiki pages |
|---|---|---|---|
| ACR | Architecture Concept Review | Architecture definition process | |
| ADD | Architecture Definition Document | ADD Rev C | |
| ALARA | As Low As Reasonably Achievable | Technology Gaps | #0308 |
| APH | Advanced Plant Habitat | Technology Gaps | #0305 |
| ARMADAS | Automated Reconfigurable Mission Adaptive Digital Assembly Systems | Technology Gaps | #0504 |
| AS | Applied Science | Objective Category | Objectives |
| ASA | Australian Space Agency | Space Agency | |
| ASI | Italian Space Agency (Agenzia Spaziale Italiana) | Space Agency | |
| CAPSTONE | Cislunar Autonomous Positioning System Technology Operations and Navigation Experiment | Mission | Missions and assets |
| CaRD | Carbothermal Reduction Demonstration | Technology Gaps | #0601 |
| CLDP | Commercial Low Earth Orbit Development Program | Program | RT-8 |
| CLPS | Commercial Lunar Payload Services | Element | CLPS |
| CNES | French Space Agency (Centre National D'Etudes Spatiales) | Space Agency | |
| COTS | Commercial Off-The-Shelf | ||
| C&PNT | Communication and Positioning, Navigation, and Timing | Sub-Architecture | C&PNT Systems |
| CSA | Canadian Space Agency | Space Agency | |
| DEM | Digital Elevation Map | Data Gaps | DN-002 L |
| DLR | German Aerospace Center (Deutsches Zentrum für Luft- und Raumfahrt) | Space Agency | |
| DSAC-1 | Deep Space Atomic Clock | Technology Gaps | #0104 |
| DSN | Deep Space Network | Sub-Element | SCaN Networks |
| DSNE | Design Specification for Natural Environments | Data Gaps | DN-008 L |
| ECLSS | Environmental Control and Life Support System | ||
| EDL | Entry, Descent, and Landing | #1103 | |
| EGS | Exploration Ground Systems | Element | EGS |
| EP | Electric Propulsion | Technology Gaps | #0503 |
| ESA | European Space Agency | Space Agency | |
| ESM | European Service Module | Sub-Element | Orion |
| ESPIRIT | European System Providing Refueling Infrastructure and Telecommunication | Gateway Component | Gateway. Spelled "ESPRIT" in the Gateway pages (p. 53). |
| EVA | Extravehicular Activity | xEVA | |
| FE | Foundational Exploration | Segment | FE |
| GCR | Galactic Cosmic Radiation | Technology Gaps | #0307 |
| GDOP | Geometric Dilution of Precision | Technology Gaps | #0101 |
| GRAM | Global Reference Atmospheric Model | DN-003 M | |
| GNSS | Global Navigation Satellite System | ||
| H2M | Humans to Mars | Segment | H2M |
| HALO | Habitation and Logistics Outpost | Gateway | |
| HBS | Human and Biological Science | Objective Category | Objectives |
| HD | High Definition | Technology Gaps | |
| HDL | Human-class Delivery Lander | HDL | |
| HLR | Human Lunar Return | Segment | HLR |
| HLS | Human Landing System | Element | HLS |
| HS | Heliophysics Science | Objective Category | Objectives |
| I/O | Input/Output | Technology Gaps | |
| I-Hab | International Habitation Module | Gateway Component | Gateway |
| IM&R | Inspection, Maintenance, and Repair | Technology Gaps | #0501 |
| IPEx | ISRU Pilot Excavator | Technology Gaps | #0605 |
| ISA | Israel Space Agency | Space Agency | |
| ISRO | Indian Space Research Organization | Space Agency | |
| ISRU | In-Situ Resource Utilization | ISRU Systems | |
| IVA | Intra-Vehicular Activities | ||
| JAXA | Japan Aerospace Exploration Agency | Space Agency | Pressurized Rover |
| KASA | Korean AeroSpace Agency | Space Agency | |
| KASI | Korea Astronomy and Space Science Institute | Space Agency | |
| KPLO | Korea Pathfinder Lunar Orbiter | Mission | DN-001 L |
| LCRNS | Lunar Communication Relay and Navigation Systems | Sub-Element | SCaN Networks. "Lunar Communications Relay …" in the SCaN one-pager (p. 64). |
| LEAP | Lunar Exploration Accelerator Program | RT-1 | |
| LEO | Low Earth Orbit | RT-8 | |
| LI | Lunar Infrastructure | Objective Category | Objectives (the goals table prints "(LS)", p. 16) |
| LOLA | Lunar Orbiter Laser Altimeter | Data Gaps | DN-002 L |
| LPS | Lunar/Planetary Science | Objective Category | Objectives |
| LRO | Lunar Reconnaissance Orbiter | Mission | |
| LROC | Lunar Reconnaissance Orbiter Camera | Data Gaps | DN-001 L |
| LTV | Lunar Terrain Vehicle | Element | LTV |
| LuPEX | Lunar Polar Exploration | Mission | RT-1 |
| MBRSC | Mohammed Bin Rashid Space Centre | Space Agency | Gateway |
| MEGANE | Mars-moon Exploration with GAmma rays and NEutrons | Mission | RT-1 |
| MI | Mars Infrastructure | Objective Category | Objectives |
| NAC | Narrow Angle Camera | Data Gaps | DN-001 L |
| NASA | National Aeronautics and Space Administration | Space Agency | |
| NEP | Nuclear Electric Propulsion | Technology Gaps | #1104 |
| NPR | NASA Procedural Requirements | ||
| NRHO | Near Rectilinear Halo Orbit | Gateway; LD-04-L | |
| NSN | Near Space Network | Sub-Element | SCaN Networks |
| NTP | Nuclear Thermal Propulsion | Technology Gaps | #1104 |
| NZSA | New Zealand Space Agency | Space Agency | |
| OHRC | Chandrayaan-2 Orbiter High Resolution Camera | Data Gaps | DN-001 L |
| OP | Operations | Objective Category | Objectives |
| PL&HA | Precision Landing and Hazard Avoidance | Technology Gaps | #1101, #1102 |
| PMAD | Power Management and Distribution | Technology Gaps | #0903 |
| PNT | Positioning, Navigation, and Timing | C&PNT Systems. F.2 heads its entry "Position, Navigation, and Timing" (p. 299). | |
| PPD | Pixel/Degree | Data Gaps | DN-003 L |
| PPE | Power Propulsion Element | Gateway Component | Gateway |
| PPS | Physics and Physical Sciences | Objective Category | Objectives (the goals table has "Physics and Physical Science") |
| PR | Pressurized Rover | Element | Pressurized Rover |
| PRISM | Payload and Research Investigations from the Surface of the Moon | Solicitation | RT-1 |
| PSI | Plume Surface Interaction | Technology Gaps | #1101; DN-017 L |
| PSR | Permanently Shadowed Region | Environment; #0804 | |
| RT | Recurring Tenet | Objective Category | Recurring tenets |
| SCALPSS | Stereo Cameras for Lunar Plume-Surface Studies | Payload | DN-017 L; RT-6 |
| SCaN | Space Communications and Navigation | NASA Program | SCaN Networks |
| SE | Science-Enabling | Objective Category | Objectives |
| SEP | Solar Electric Propulsion | Technology Gaps | #1104 |
| SfS | Shape from Shading | Data Gaps | DN-018 L |
| SLE | Sustained Lunar Evolution | Segment | SLE |
| SLIM | Smart Lander for Investigating Moon | Mission | RT-1 |
| SLS | Space Launch System | Element | SLS |
| SOA | State of the Art | Technology Gaps | Gaps index |
| SPE | Solar Particle Event | Technology Gaps | #0307 |
| SSA | Saudi Space Agency | Space Agency | |
| SWaP | Size, Weight, and Power | ||
| TLT | Tall Lunar Tower | Technology Gaps | #0504 |
| TH | Transportation and Habitation | Objective Category | Objectives |
| TOCA | Total Organic Carbon Analyzer | Technology Gaps | #0304 |
| TRL | Technology Readiness Level | Technology Gaps | Gaps index |
| TRN | Terrain Referenced Navigation | Data Gaps | DN-002 L |
| TTC | Telemetry, Tracking, and Command | Technology Gaps | #1003 |
| UHF | Ultra High Frequency | Technology Gaps | |
| VEGGIE | Vegetable Production System | Technology Gaps | #0305 |
| VIPER | Volatiles Investigating Polar Exploration Rover | Technology Gaps | Missions and assets |
| WEH | Water Equivalent Hydrogen | Data Gaps | DN-006 L |
| xEVA | Exploration EVA Systems | Element | xEVA (heading: "Exploration EVA System") |
| 3GPP | 3rd Generation Partnership Project | Technology Gaps | #0103; LD-103 |
Notes on F.1:
- "Usage/Context" says where in the ADD a term comes up, not what kind of thing it is. VIPER, a rover, is tagged "Technology Gaps"; RT, the recurring tenets, "Objective Category"; NASA "Space Agency". HALO and HDL have no tag, while PPE and I-Hab are "Gateway Component" and the other elements "Element" (the wiki's reading of the column).
- Spellings that differ from the body. "ESPIRIT" here, "ESPRIT" in the Gateway pages (p. 53); "Lunar Communication Relay" here, "Lunar Communications Relay" on p. 64. The 2023 executive overview also prints "ESPIRIT" (open question 56).
- Expanded in the body but not listed: ESDMD, "Exploration Systems Development Mission Directorate" (p. 12); AxEMU, "Axiom Extravehicular Mobility Unit" (p. 48); CEV, "Crew Exploration Vehicle", and ESAS, "Exploration Systems Architecture Study" (both p. 191). The ADD never expands the LD and MD prefixes of its definition tasks, here or in Appendix C (Key definition tasks).
- The wiki's own ID formats (UC-, FN-, DN-, the four-digit gap numbers) aren't acronyms in F.1. How to read them is on Use cases and functions, the gaps index and the data gaps index.
Terms (F.2)¶
F.2, "Glossary of Terms" (pp. 295–303), in the printed order. Fourteen entries end "(Definition from Moon to Mars Strategy and Objectives)"; the table marks them "M2M S&O" instead of repeating it. Two others cite a source of their own (the Systems Engineering Handbook; NPR 7120.5). The order is mostly alphabetical. Out-of-place entries include "Explore" before "Exploration Asset" and "Function" before "Frozen Samples" (p. 297), "Large Cargo" before "Large Asset" (p. 298), "Scalability" after "Semi-Autonomous System" (p. 301), "Definition Task", "Definition Outcome" and "Trade Space" between "System" and "Transit", and "Traverse" before the two "To Be" entries (p. 302). Pp. 298 and 301–302 were checked against the PDF; p. 297 is from the text layer.
| Term | NASA's definition | p. | Notes and wiki pages |
|---|---|---|---|
| Architecture | "The high-level unifying structure that defines a system. It provides a set of rules, guidelines, and constraints that defines a cohesive and coherent structure consisting of constituent parts, relationships and connections that establish how those parts fit and work together." | 295 | "(Definition from NASA's System Engineering Handbook)". Architecture framework; compared below |
| Architecture-driven Data Gap | "Data the agency needs to advance the Moon to Mars Architecture that is not met by any existing information." | 295 | Data gaps index (Section 3.3 has nearly the same words, p. 80). No entry for technology gaps. |
| Artemis Mission | "The crewed portion of an Artemis Mission Campaign, beginning at crew liftoff from Earth and ending at crew return to Earth." | 295 | |
| Artemis Mission Campaign | "A collective grouping of uncrewed missions and their associated crewed mission." | 295 | |
| Automation | "Automatically controlled operation of an apparatus, process, or system by mechanical or electronic devices that take the place of human labor (e.g., computer control of a docking operation or vehicle surface traverse). Human intervention can be available, as determined by hazard controls (e.g., breakout or transition to safe mode), but not required to complete an automated operation." | 295 | Autonomous Systems and Robotics |
| Autonomous System | "A combination of elements that function together to achieve goals while operating independently of external controls. An autonomous system may involve any combination of elements (e.g., humans and machines) and is not limited to uncrewed capability." | 295 | as above |
| Autonomy | "The ability of a system to achieve goals while operating independently of external controls. Autonomy does not preclude external reprioritization or generation of new goals. It only requires execution of existing goals without external control." | 295 | as above |
| Baseline | "An agreed-to set of requirements, designs, or documents that will have changes controlled through a formal approval and monitoring process." | 295 | |
| Campaign | "A series of interrelated missions that together achieve Agency goals and objectives." | 295 | M2M S&O |
| Cargo | "Items that are transported from one location to another." | 295 | Redefined in Rev A.1 (pp. 3–4); see below |
| Carrier | "A transport structure or container used to secure and protect logistics items that require transport to the point of use." | 295 | Logistics Systems; LD-102 |
| Characteristics | "Features or activities of exploration mission implementation that are necessary to satisfy the goals and objectives." | 295 | Objective decomposition; compared below |
| Cislunar Space | "The region of space from the Earth to the Moon. Specifically for the Moon to Mars Architecture, elements under the influence of lunar gravity, beyond Earth's geosynchronous orbit and inclusive of low lunar orbit but distinct from the lunar surface." | 295 | |
| Co-Manifested Payload | "Cargo on a transportation element utilizing excess volume and mass (e.g., cargo located inside the payload attach fitting adapter ring)." | 295 | |
| Concept of Operations | "Developed early in Pre-Phase A, describes the overall high-level concept of how the system will be used to meet stakeholder expectations, usually in a time-sequenced manner. It describes the system from an operational perspective and helps facilitate an understanding of the system goals. … It serves as the basis for subsequent definition documents and provides the foundation for the long-range operational planning activities (for nominal and contingency operations). It provides the criteria for the validation of the system. …" | 295–296 | Shortened here. The full entry also says it "stimulates the development of the requirements and architecture related to the user elements of the system" and "becomes part of the concept documentation". |
| Consumables | "Supplies (not including propellant) that are needed to support mission activities." | 296 | Same words as "Logistic Items"; redefined in Rev A.1 (pp. 3–4) |
| Continuous Presence | "Steady cadence of human/robotic missions in subject orbit/surface with the desired endpoint of 24/7/365 operations." | 296 | M2M S&O. The 2022 wording has "365/24/7" (below) |
| Control Mass | "Used to define the capability and baseline architecture of the system. It represents the controlled, not-to-exceed allocation of mass to an element." | 296 | |
| Crew Countermeasure System(s) | "Systems that enable aerobic and resistance exercise for crew inside habitable assets." | 296 | #0401 |
| Cryogenic Samples | "Samples that are typically below -153°C/120K." | 296 | #1201, whose targets leave the ranges TBR |
| Deep Space Environments | "Deep space is the vast region of space that extends to interplanetary space, to Mars and beyond. It is the region of space beyond Earth's Moon, including Lagrange 2, or L2, (274,000 miles from Earth). This environment has many defining factors, including harsh radiation (both solar particle events and galactic cosmic rays), space weather, and microgravity." | 296 | B.1's note on "deep space" (p. 109): Use cases and functions |
| Deep Space Transport | "Deep Space Transport is used to describe the assembled Mars transit vehicle stack, which will consist of a propulsion and power transportation system backbone and attached cargo. There are two Deep Space Transport variants: in the crew variant, the cargo will consist of a transit habitat that may or may not be a separate free-flyer that docks with transport; in the cargo variant, the cargo will consist of orbital assets to be delivered to Mars orbit, or surface assets mounted to Mars descent systems that will be delivered to the Mars surface." | 296 | #1104; Humans to Mars |
| Deep Sub-Surface Samples | "Samples collected from locations 10–100m below the lunar or Martian surface." | 296 | |
| Demonstrate | "Deploy an initial capability to enable system maturation and future industry growth in alignment with architecture objectives." | 296 | M2M S&O; develop or demonstrate |
| Deploy | "To move into place or bring into effective action." | 296 | |
| Develop | "Design, build, and deploy a system, ready to be operated by the user, to fully meet architectural objectives." | 296 | M2M S&O |
| Earth Vicinity | "The region of space around the Earth-Moon system, including cislunar space, low Earth orbit, and orbits around the Earth-Moon barycenter." | 296 | |
| Effectivity | "The conditions or mission for which a requirement is initially applicable." | 296 | |
| Element | "Any exploration system that enables a high-level functional allocation (e.g., crew transport, habitation, logistics delivery) that is primarily self-sufficient." | 296 | Elements |
| Excursion | "The activity of moving to and/or returning from a location on the lunar surface through extravehicular operations and/or surface mobility assets." | 297 | Mobility Systems |
| Explore | "Excursion-based expeditions focused on science and technology tasks." | 297 | M2M S&O |
| Exploration Asset | "All items that are in place and being used as part of the exploration architecture." | 297 | Elements; p. 21 adds "including payloads" |
| Exploration Strategy | "Establish the scenarios, conceptual missions, and systems needed to extend humanity's reach beyond low Earth orbit, return to the Moon, and proceed on toward Mars and beyond." | 297 | |
| Function | "Actions that an architecture would perform that are necessary to complete the desired use case." | 297 | Use cases and functions; p. 17 lacks "that are necessary" |
| Frozen Samples | "Samples that are typically around the -85°C range." | 297 | #1201 |
| Global | "Infrastructure and capabilities that support human and robotic operations and utilization across the subject planetary surface." | 297 | M2M S&O |
| Gravity | "'Gravity' refers to acceleration on Earth (~9.81 ms−2), and is expressed in the international system of units (SI) as g. A gravity level lower than 1 g is called 'partial gravity' or 'reduced gravity'." | 297 | |
| Habitable Environment | "The environment that is necessary to sustain the life of the crew and to allow the crew to perform their functions in an efficient manner." | 297 | Habitation Systems |
| Human Landing System Initial Configuration | "Any crewed mission to the lunar surface executed with the initial HLS configurations as defined in the HLS Broad Agency Announcement Option A. (Effectivity for requirements unique to this configuration are noted as 'HLS Initial Configuration.')" | 297 | HLS |
| Human-Rating | "A human-rated system accommodates human needs, effectively utilizes human capabilities, controls hazard with sufficient certainty to be considered safe for human operations, and provides, to the maximum extent practical, the capability to safely recover the crew from hazardous situations. Human-rating consists of three fundamental tenets: Human-rating is the process of designing, evaluating, and assuring that the total system can safely conduct the required human missions. Human-rating includes the incorporation of design features and capabilities that accommodate human interaction with the system to enhance overall safety and mission success. Human-rating includes the incorporation of design features and capabilities to enable safe recovery of the crew from hazardous situations." | 297 | RT-3 Crew Return |
| Hybrid Propulsion System | "A vehicle consisting of two or more unique propulsion systems, each optimized for different types of maneuvers. For the purpose of this document, two hybrid systems are considered: solar electric propulsion/chem, which combines a solar electric propulsion system with a chemical stage, and Nuclear Electric Propulsion/chem, which combines a nuclear electric propulsion system with a chemical stage." | 297 | #1104 |
| Increment | "The period of time between the end of one crew mission (i.e., crew splashdown) and the end of a second crew mission, including the uncrewed activities and operations that commence during this defined timeframe." | 297 | |
| Incremental | "Building compounding operational capabilities within the constraints of schedule, cost, risk, and access." | 298 | M2M S&O |
| Integrated Element | "A portfolio that comprises multiple individual assets and provides a suite of integrated capabilities, offering flexible, evolvable concepts to achieve NASA's Moon to Mars Objectives." | 298 | The body uses the phrase once, for the SCaN Networks: "this integrated element" (p. 64; the wiki's search). See open question 32. |
| Interoperability | "The ability of two or more systems to physically interact; exchange data, information, or consumables; or share common equipment while successfully performing intended functions." | 298 | RT-7 Interoperability |
| Intravehicular Activity Facilities | "Facilities inside a habitable asset, sustained across crewed and uncrewed increments, that allow the hosting and operation of dedicated utilization payloads." | 298 | |
| Key Architecture Definition Task | "An architecture definition task that influences the end-to-end architecture and warrants elevated scrutiny." | 298 | Key definition tasks; compared below |
| Large Cargo | "Items greater than 6t in mass that are transported from one location to another." | 298 | Rev A.1 "removed 'large cargo' from glossary" (pp. 3–4); below |
| Large Asset | "For lunar, an asset that is greater than 6t in mass." | 298 | #0808 Relocation of Large Assets |
| Legacy Decision | "A decision made before the implementation of the architecture decision roadmapping process." | 298 | Key definition tasks |
| Limited Capability Mission | "A mission to a polar landing site where the utilization capability of the mission is limited to the threshold capabilities of HLS and Orion, with no additional delivery or return mass available from goal capabilities or other elements. Additionally, certain missions may prioritize crew time and transportation mass to the delivery and outfitting of new elements in NRHO (e.g., Gateway elements) or the lunar surface (e.g., Pressurized Rover and initial surface habitat). For the purposes of analysis, a two-crew, 6.5-day sortie was assumed as a representative case. … Thus, this mission category represents a case in which only a threshold of utilization activities is expected to be performed." | 298 | Shortened here; the omitted lines say crew time for "ingress, setup, outfit, and checkout" of new elements and their logistics mass leave less for utilization. Compare LD-07-L's sortie of "around 6 days" (p. 191). |
| Live | "The ability to conduct activities beyond tasks on a schedule. Engage in hobbies, maintain contact with friends and family, and maintain healthy work-life balance." | 298 | M2M S&O |
| Logistics | "Capabilities associated with packaging, handling, storage, transportation, and tracking of logistics items and goods not initially delivered as part of an exploration element, including equipment, tools, consumables, maintenance items, spares, and subsystem components needed to support mission activities such as operations, outfitting, science, research, and utilization. Logistics also includes capabilities associated with reuse, recycling, and disposal of trash and waste." | 298 | Logistics Systems |
| Logistic Items | "Supplies (not including propellant) that are needed to support mission activities." | 298 | Same words as "Consumables" |
| Loss of Crew | "Death of or permanently debilitating injury to one or more crew members." | 299 | MD-04 (Key definition tasks) |
| Loss of Mission | "Loss of or inability to complete significant/primary mission objectives, which includes loss of crew. Each mission is defined with different assumptions and mission objectives. Therefore, specific mission loss-of-mission assessments are accomplished evaluating the attainment of specific mission objectives, using methods tailored to the specific mission risk drivers and each specific program but consistent with defined NASA Probabilistic Risk Assessment standards." | 299 | MD-08 (open) |
| Maintenance | "The function of keeping items or equipment in, or restoring them to, a specified operational condition. It includes servicing, test, inspection, adjustment/alignment, removal, replacement, access, assembly/disassembly, lubrication, operation, decontamination, installation, fault location, calibration, condition determination, repair, modification, overhaul, rebuilding, and reclamation. Preventative maintenance is performed before a failure occurs, whereas corrective maintenance occurs in response to a failure." | 299 | RT-5 |
| Mechanical Assistance | "Device intended to allow the crew to transport more mass than they can hand carry while walking." | 299 | Mobility Systems |
| Mission | "A major activity required to accomplish an agency goal or to effectively pursue a scientific, technological, or engineering opportunity directly related to an Agency goal. Mission needs are independent of any particular system or technological solution." | 299 | M2M S&O |
| Mobility | "Powered surface travel that extends the exploration range beyond what is possible for astronauts to cover on foot. Spans robotic and crewed systems and can be accomplished on and above the surface." | 299 | M2M S&O; Mobility Systems |
| Near-Surface Samples | "Samples collected from locations 1–2m below the lunar or Martian surface." | 299 | |
| Needs | "A statement that drives architecture capability, is necessary to satisfy the Moon to Mars objectives, and identifies a problem to be solved, but is not the solution." | 299 | Objective decomposition |
| Permanently Shadowed Regions | "Areas of the lunar surface that never receive direct sunlight (or have not seen direct sunlight in billions of years). These extremely cold regions, often found in craters near the lunar poles, can contain frozen volatiles of interest for lunar science and ISRU." | 299 | Environment |
| Planetary Protection | "Approaches used to avoid harmful contamination of solar system bodies during exploration activities, as well as avoiding possible harmful extraterrestrial contamination from material that may be returned from other solar system bodies, in compliance with Outer Space Treaty constraints." | 299 | Planetary protection, where the ACR25 paper defines forward and backward separately |
| Position, Navigation, and Timing | "Position, navigation, and timing (PNT) encompasses the ability to enable broad awareness of a user's location in space and time. Accomplishing PNT relies on both infrastructure and user capabilities. Infrastructure includes the critical foundations of lunar reference system components and lunar reference time, and the sources provided by a broad suite of network assets that rely on those foundations. … Together these foundational elements, radionavigation sources, and user-provided sensors enable a user, either in orbit or on the surface, to maintain awareness of their position, velocity, and time." | 299–300 | Shortened here. C&PNT Systems |
| Powered Mobility Asset | "Asset that allows the crew to travel further distances than they can walk (e.g., Lunar Terrain Vehicle or Pressurized Rover)." | 300 | LTV; Pressurized Rover |
| Priority Key Definition Task | "A key definition task with many flow-down impacts upon subsequent tasks and which therefore was presented and approved at the Architecture Concept Review to be made early in the architecture roadmapping process." | 300 | Key definition tasks |
| Reconfiguration | "If a system is required to provide a function, any time required by the crew associated with making that function available for use, including changing spaces and moving logistics to allow for use of the space for a different purpose (e.g., exercise, eating, sleeping, medical, training, working)." | 300 | RT-4 Crew Time |
| Reference Mission | "A defined set of elements with assumed functional allocations working together in a focused mission context that serves as a common point of comparison for strategic analysis and early program formulation activities (prior to Authority to Proceed) and will be updated when necessary to remain in alignment with the overall exploration goals and objectives." | 300 | Segments |
| Reference System | "A theoretical system of coordinates and standards sufficient to define the position and motion of objects in space and time. A reference system is composed of a specified origin, the directions of fundamental axes, and a set of conventional models, procedures, and constants used to realize the system." | 300 | C&PNT Systems (the 2024 reference-frames paper) |
| Refrigerated Samples | "Samples that typically need to be maintained in the +4°C to -20°C range." | 300 | #1201 |
| Reposition/Relocate | "The act of moving cargo from one location to another on the lunar or Martian surface." | 300 | |
| Robotic Systems | "Systems intended to interact with their environment and/or objects in the environment through powered motions and a controlled relationship between sensing and action. Robotic systems can perform physical tasks (e.g., manipulating or moving objects, mobility across terrain), and they may or may not exhibit some degree of autonomy. Habitation and transportation systems (as defined by those sub-architectures) and disembodied autonomous systems that lack the capacity for physical interaction are not robotic systems." | 300 | Autonomous Systems and Robotics |
| Routine | "Recurring subject operations performed as part of a regular procedure rather than for a unique reason." | 300 | M2M S&O |
| Routine Preventative Maintenance | "Planned maintenance done on a regular (daily, weekly, monthly) basis that is part of the design, such as filter changes, lubrication, cleaning, etc." | 300 | |
| Samples/Commodities/Logistics Items | "Samples, commodities, and supplies (not including propellant) that are needed to support mission activities." | 300 | |
| Secondary Payloads | "Additional cargo carried on a transportation element, currently on an adapter ring, after the primary and co-manifested payloads are accommodated, limited by the remaining transportation element resources (e.g., mass, volume, power)." | 301 | |
| Semi-Autonomous System | "A system that operates independent of external control in the execution of a subset of its operational goals or task objectives while relying on operator control input (from crew and/or ground) for its complete end-to-end operations (i.e., a system that shares control with an external operator, exhibiting autonomy over some, but not all, of its operational goals/objectives)." | 301 | Autonomous Systems and Robotics |
| Scalability | "Initial systems designed such that minimal recurring DDT&E is needed to increase the scale of a design to meet end state requirements." | 301 | M2M S&O. DDT&E is not in F.1. |
| Segments | "A portion of the architecture, identified by one or more notional missions or integrated use cases, illustrating the interaction, relationships, and connections of the sub-architectures through progressively increasing operational complexity and objective satisfaction." | 301 | Segments; Architecture framework |
| Small Asset | "For lunar other, non-utilization assets less than 6t in mass. Excludes utilization payloads, utilization equipment, and samples/commodities/logistics items." | 301 | "For lunar other" as printed (PDF checked) |
| Small Cargo | "Any item less than 6t in mass that is transported from one location to another, including utilization payloads and equipment, small assets, or samples/commodities/logistics items." | 301 | |
| Sol | "Martian day, approximately 24 hours and 39 minutes long. For the purpose of this document, operational timekeeping on the surface of Mars uses Martian sols to align with the Martian day/night cycle." | 301 | |
| Sortie Missions | "A single crewed mission to a lunar surface location for a period of days supported solely by the lunar crewed lander. The main characteristics of the sortie mission are that crew habitation is provided by the crewed lander and the crew can perform all lunar surface activities using self-contained resources—although pre-deployment of resources is not necessarily precluded during a sortie mission." | 301 | HLS |
| Stakeholder | "An organization with an interest in a particular architecture definition task because it can either affect or be affected by the definition outcome. Different architecture definition tasks may have different stakeholders who are responsible for contributing supporting data and analyses. In some cases, stakeholders are authorities for prerequisite definition tasks that feed into a particular key definition task." | 301 | Key definition tasks |
| Stage | "Provide an area in which participants and logistics are brought together and readied for an activity." | 301 | |
| Stow | "Provide physical space for the storage of items, usually samples that have been collected and placed in containers." | 301 | |
| Sub-Architecture | "A group of tightly coupled elements, functions, and capabilities that perform together to accomplish architecture objectives." | 301 | Sub-architectures |
| Sub-Surface Samples | "Samples collected from locations 2–10m below the lunar or Martian surface." | 301 | |
| System | "The combination of elements that function together to produce the capability required to meet a need. The elements include all hardware, software, equipment, facilities, personnel, processes, and procedures needed for this purpose." | 302 | "(Refer to NPR 7120.5.)" |
| Definition Task | "An examination of a question within the architecture, typically to shape or reduce the trade space." | 302 | Compared below |
| Definition Outcome | "The result of an architecture definition task, which could include a decision, down-select, ground rule, methodology, or other narrowing of the trade space." | 302 | as above |
| Trade Space | "An exploratory part of the systems engineering process that identifies and analyzes potential solutions for an architectural concept, function, or component. The trade space includes assessments of state-of-the-art and anticipated future capabilities applied as part of a range of solutions, and assessments of impacts that each solution could have across a system's development lifecycle or the architecture as a whole." | 302 | Defined differently in Appendix C and the white paper (below) |
| Transit | "The carrying of people, goods, or materials from one place to another in space." | 302 | |
| Transport | "The act of moving crew or cargo from one location to another in space." | 302 | |
| Traverse | "To travel across or over the surface." | 302 | |
| To Be Determined (TBD) | "Used when the value to be placed in a requirement is not known and there is open work to determine what it should be." | 302 | Common in gap targets (gaps index) |
| To Be Resolved (TBR) | "Used when a value for a requirement is presented but it is to be resolved or refined as to whether it is the right number." | 302 | as above |
| Use Case | "Operations that would be executed to produce the desired needs and/or characteristics." | 302 | Use cases and functions |
| User Burden | "The demands imposed on exploration elements or assets seeking to access a service or capability (e.g., for missions or systems accessing C&PNT sub-architecture services)" | 302 | C&PNT Systems |
| Utilization | "Use of the platform, campaign, and/or mission to conduct science, research, test and evaluation, public outreach, education, and industrialization." | 302 | M2M S&O; Utilization Systems |
| Utilization Mass | "The mass of utilization payloads." | 302 | |
| Utilization Payloads and Equipment | "Any item that is primarily in support of and attributed to utilization objectives. Utilization payloads include science/research payloads and technology demonstrations. Equipment includes other internal and external hardware, supporting tools, supplies, etc." | 302 | Elements |
| Validate | "Confirming that a system satisfies its intended use in the intended environment (i.e., did we build the right system?)." | 302 | M2M S&O |
| Verification (of a product) | "Proof of compliance with a requirement. Verification may be determined by testing, analysis, demonstration or inspection." | 302 | |
| Volatiles | "Elements, molecules, and compounds that readily vaporize, converting to their gaseous form (e.g., water and carbon dioxide). To preserve the scientific integrity of these materials, sample return efforts require preservation of their native environmental conditions (e.g., cold conditioning)." | 302 | DN-013 L; #1201 |
| Work Time | "Non-personal time. Time during which the crew is in a duty status (e.g., typically 8–8.5 hours, but could be 11.5 hours for an EVA day or other mission-specific extension)." | 303 | RT-4 Crew Time |
Entries that overlap inside Appendix F¶
- Consumables, Logistic Items, Samples/Commodities/Logistics Items. The first two have the same words, "Supplies (not including propellant) that are needed to support mission activities" (pp. 296, 298); the third adds samples and commodities (p. 300). Rev A.1 (March 2024) "Updated definitions of 'cargo' and 'consumables'" (revision history, pp. 3–4).
- Large and small, at 6 t. Large Cargo and Large Asset are over 6 t; Small Cargo and Small Asset under (pp. 298, 301). F.3 uses the same line for "Large Exploration Assets" (p. 304). Rev A.1's entry says it "removed 'large cargo' from glossary" (pp. 3–4), but Rev C's glossary has a "Large Cargo" entry (p. 298). The ADD doesn't say when it came back (open question 21).
- Two sortie-type missions. "Sortie Missions" are supported "solely by the lunar crewed lander" (p. 301). A "Limited Capability Mission" assumes "a two-crew, 6.5-day sortie" (p. 298). LD-07-L puts early sorties at "around 6 days", to match "the NRHO orbit of around 6.5 days" (p. 191).
- Transit and Transport. "The carrying of people, goods, or materials" against "The act of moving crew or cargo", both "from one place to another in space" or "from one location to another in space" (p. 302). "Reposition/Relocate" is the surface counterpart for cargo (p. 300).
- Samples by depth and temperature. Near-surface 1–2 m, sub-surface 2–10 m, deep sub-surface 10–100 m (pp. 296, 299, 301). Refrigerated +4 °C to -20 °C, frozen around -85 °C, cryogenic below -153 °C/120 K (pp. 296, 297, 300). Gap #1201 still gives its storage temperatures as TBR; the F.2 values are not in its table (the wiki's comparison).
Quantity descriptors (F.3)¶
"The following descriptors define terms used in the objective decomposition; they capture approximate quantities for terms like small, medium, and large, etc." (p. 304). Five small tables, merged here (PDF checked):
| Activity (table heading) | Term | Description |
|---|---|---|
| Transport of cargo to the lunar surface | Limited Amount | 100s of kg |
| Moderate Amount | 1000s of kg | |
| Large Exploration Assets | Assets greater than 6t in mass | |
| Transport of cargo from the lunar surface | Small Amount | 10s of kg |
| Large Amount | 100s of kg | |
| Unloading of cargo | Limited Amount | 100s of kg |
| Moderate Amount | 1000s of kg | |
| Large Exploration Assets | Assets greater than 6t in mass | |
| Repositioning of cargo | Limited Amount | 100s of kg |
| Moderate Amount | 1000s of kg | |
| Exploration Assets | Assets greater than 6t in mass | |
| Repositioning of samples and containers | Small Amount | 10s of kg |
| Large Amount | 100s of kg |
Notes (the wiki's reading):
- No "medium". The introduction names "small, medium, and large", but no table uses "medium"; "limited" and "moderate" take its place. The repositioning table says "Exploration Assets" where the others say "Large Exploration Assets", for the same 6 t line.
- Where the words appear. The lunar use-case and function titles carry them with the quantity in brackets, for example FN-T-201 L "Transport a limited amount of cargo (100s of kg) from Earth to south pole region sites on the lunar surface" and FN-T-202 L, "a moderate amount of cargo (1000s of kg)" (Lunar functions).
- Two element descriptions use "moderate". The Lunar Utility Rover "can also transport a moderate amount of cargo (thousands of kg)" (p. 61), which matches F.3. The Lunar Surface Cargo Lander delivers "moderate amounts of cargo to the lunar surface" with no figure (p. 59). F.3 says it defines terms "used in the objective decomposition", not in element descriptions, so the wiki doesn't size the lander from it (open question 58).
Same word, other definitions¶
The ADD defines some terms twice: in Sections 1–2 or Appendix C, and again in Appendix F. Some are also defined in the white papers, the objectives documents and the executive overviews. Where F differs from the body of the same document, neither is newer, so the wiki records both. The comparisons are the wiki's.
The building blocks: Appendix F against Sections 1 and 2¶
| Term | Appendix F | ADD body | What differs |
|---|---|---|---|
| Architecture | "The high-level unifying structure that defines a system …" (p. 295) | "the high-level, unifying structure that defines a system …" (p. 11), from the Systems Engineering Handbook | Same definition, same source; punctuation and "defines"/"define" only |
| Characteristics; Needs | Two entries: "Features or activities of exploration mission implementation that are necessary to satisfy the goals and objectives" (p. 295); "A statement that drives architecture capability …" (p. 299) | One entry, "Characteristics and needs": "Features to satisfy the goals and objectives; statements that drive architecture capability …" (p. 17) | F splits the term and adds "activities" and "necessary" to the first half |
| Use Case | "Operations that would be executed to produce the desired needs and/or characteristics." (p. 302) | Same words (p. 17) | none |
| Function | "Actions that an architecture would perform that are necessary to complete the desired use case." (p. 297) | "Actions that an architecture would perform to complete the desired use case." (p. 17) | F adds "that are necessary" |
| Segments | "A portion of the architecture …" (p. 301) | "Portions of the architecture …" (pp. 18, 21) | singular against plural; otherwise the same |
| Sub-Architecture | as on p. 301 | Same words (pp. 18, 21) | none |
| Element | as on p. 296 | Same words (p. 21) | none |
| Exploration Asset | "All items that are in place and being used as part of the exploration architecture." (p. 297) | "Any item that is in place and being used as part of the exploration architecture, including payloads." (p. 21) | F drops "including payloads" |
| Utilization Payloads and Equipment | as on p. 302 | Same words (p. 21) | none |
| Utilization | "Use of the platform, campaign, and/or mission …" (p. 302) | "the use of a platform, campaign, and/or mission …" (p. 21, footnote 8) | "the" against "a" |
Against the executive overviews. The 2023 and 2024 overviews print a shorter seven-term box (Architecture, Characteristics & Needs, Use Case, Function, Element, Sub-architecture, Segment), compared with the ADD body on the 2024 overview's source page. Appendix F follows the ADD body, not the box, for Architecture, Use Case, Element, Sub-Architecture and Segments. For two terms it shares words with the box that p. 17 lacks: the box's "Features, activities, and capabilities necessary to satisfy goals and objectives" and F's "Features or activities … necessary to satisfy the goals and objectives"; the box's "An action necessary to satisfy a use case" (2024) and F's "Actions … that are necessary to complete the desired use case" (2023 overview, PDF p. 3; 2024 overview, PDF p. 20).
Definition-task terms: Appendix C, Appendix F and the white paper¶
Appendix C opens with its own "key roadmapping terms" table (p. 186). Appendix F defines most of the same terms again, and the ACR25 "Architecture Definition" white paper has a key-terms table too (WP p. 2; transcribed on Architecture definition process). All three are from December 2025.
| Term | Appendix C table (p. 186) | Appendix F | White paper (p. 2) and ADD Section 3 |
|---|---|---|---|
| (Architecture) definition task | "An examination of an open question or trade within the architecture." | "An examination of a question within the architecture, typically to shape or reduce the trade space." (p. 302) | WP: as F, plus "(e.g., trade studies in ser-vice to Moon to Mars Architecture definition)" |
| Definition outcome | "The result of a definition task, which could include a decision, down-select, ground rule, methodology, or other narrowing of the trade space." | "The result of an architecture definition task …", otherwise the same (p. 302) | WP: as F |
| Trade space | "The range of options for a particular area of the architecture." | "An exploratory part of the systems engineering process that identifies and analyzes potential solutions for an architectural concept, function, or component …" (p. 302) | WP: "A range of possible options for implementation for a particular area of the architecture." ADD p. 72: "the trade space — the range of options for exploration missions". NASA's Mars trade space web page: "the range of possibilities for a mission or campaign" (source page, "Introduction"). |
| Key definition task | "A definition task that so profoundly influences the end-to-end architecture that it warrants elevated scrutiny." | "Key Architecture Definition Task": "An architecture definition task that influences the end-to-end architecture and warrants elevated scrutiny." (p. 298) | ADD p. 72: key tasks "significantly influence the end-to-end architecture and flow down to impact many other areas of the trade space" |
| Priority key definition task | "… which was therefore presented and approved at the Architecture Concept Review to be made early in the architecture process." | "… which therefore was presented and approved … early in the architecture roadmapping process." (p. 300) | WP p. 4: "the 'priority' key definition tasks, which should be made early in the architecting process" |
| Legacy decision | "A decision made before the implementation of the architecture roadmapping process." | "… before the implementation of the architecture decision roadmapping process." (p. 298) | ADD p. 74: "decisions NASA made prior to the initial publication of the Architecture Definition Document" |
| Roadmapping; Guiding Questions; Trade Studies | not defined | not defined | WP only |
| Stakeholder | not defined | defined (p. 301) | — |
What the wiki reads from the table:
- "Trade space" is the one real difference. Appendix C, the white paper, Section 3 and NASA's Mars trade space web page make it a range of options or possibilities; Appendix F makes it "an exploratory part of the systems engineering process", closer to what the white paper calls "Trade Studies". The rest differ only in wording.
- "Decision roadmapping" survives in Appendix F. Rev C renamed "architecture decisions" to "architecture definition" (p. 4), and the 2024 executive overview's "decision roadmapping" became "architecture roadmapping" (Key definition tasks). F's "Legacy Decision" keeps the older phrase; Appendix C's table doesn't.
- "Legacy" by two yardsticks. The tables say before the roadmapping process; Section 3 says before the first ADD. The ADD doesn't say whether these are the same date.
These are recorded in open question 21.
The objectives glossary terms¶
The 2022 Moon to Mars Objectives defines 15 words used in the objectives, transcribed with their 2023 variants on Objectives. Appendix F carries 14 of them, each ending "(Definition from Moon to Mars Strategy and Objectives)". That title matches neither document's exactly (the 2022 Moon to Mars Objectives, the 2023 Strategy and Objectives Development).
- Architecture is the fifteenth, and F replaces it with the Systems Engineering Handbook definition (above). The objectives documents' "A set of functional capabilities, their translation into elements …" is not in Rev C's glossary (Architecture framework).
- F follows the 2022 wording, not the 2023 variants. It has Incremental without "to achieve a goal", Continuous Presence with "desired endpoint" rather than "desired future state", and Scalability with "DDT&E" not spelled out (2022, p. 12; 2023, PDF p. 33).
- One reordering: Continuous Presence ends "24/7/365 operations" in F (p. 296) and "365/24/7 operations" in 2022 (p. 12).
- The rest match the 2022 wording apart from capitals ("Agency goals" in Campaign; "an agency goal" once in Mission), commas (Mobility, Utilization) and "i.e.," added in Validate.
Other terms defined elsewhere¶
- Architecture-driven data gap. F: "Data the agency needs to advance the Moon to Mars Architecture that is not met by any existing information" (p. 295). Section 3.3: "data the agency needs to advance the Moon to Mars Architecture but that is not met by any existing information" (p. 80; data gaps index).
- Deep space. F: "the vast region of space that extends to interplanetary space, to Mars and beyond. It is the region of space beyond Earth's Moon, including Lagrange 2" (p. 296). B.1: "the vast region of space that extends to interplanetary space, including Mars and beyond" (p. 109; Use cases and functions). F also defines "Cislunar Space" and "Earth Vicinity" (pp. 295–296), but not B.1's "Mars vicinity".
- Planetary protection. F gives one definition covering both directions, "in compliance with Outer Space Treaty constraints" (p. 299). The ACR25 planetary protection paper defines "Forward Planetary Protection" and "Backward Planetary Protection" separately, as kinds of contamination (Planetary protection).
What Appendix F leaves out¶
- "Technology gap". F defines "Architecture-driven Data Gap" but has no entry for technology gaps. Section 3.2 defines them (p. 77; gaps index).
- "Data need" (p. 80) and "Mars vicinity" (p. 109). B.1 says "Appendix E captures additional terms and definitions" (p. 109); Appendix E is the data-gap catalog, and Appendix F doesn't define "Mars vicinity" either (open question 21).
- "Roadmapping", defined only in the white paper (WP p. 2).
- Moon Base terms. Appendix F is from December 2025; the Moon Base was announced in March 2026. The Moon Base phases and their terms are on the Moon Base hub.
- The LD and MD prefixes and DDT&E, used but never expanded (above).
Related pages¶
Objectives: words the objectives use · Architecture framework · Objective decomposition · Use cases and functions · Elements · Key definition tasks · Architecture definition process · ADD Rev C source page · 2024 executive overview
Sources¶
ADD Rev C, pp. 3–4, 11, 12, 16, 17, 18, 21, 48, 53, 59, 61, 64, 72, 74, 77, 80, 109, 186, 191, 291–304 · "Architecture Definition" white paper, pp. 2, 4 · Moon to Mars Objectives (2022), p. 12 · Strategy and Objectives Development (2023), PDF p. 33 · 2023 executive overview, PDF p. 3 · 2024 executive overview, PDF p. 20 · ACR25 planetary protection white paper, p. 1