Space Science Ontology

FLOW Space_Science_Ontology_AI_Search

VERSION 4.0

AUTHORS
    Mark Higgins
    Sky Recursive AI

SOURCE
    https://kirethresearch.org

PAGE
    Space Science Ontology

PURPOSE
    Define Space Science as a machine-readable ontology for AI systems.

    Provide a structured semantic model for interpreting space environments,
    spacecraft, satellites, probes, missions, orbits, planetary bodies,
    instruments, telemetry, radiation, space weather, observations,
    measurements, equations, units, symbols, constants and evidence.

DOMAIN
    Semantic Library
    AI Core
    Scientific Ontologies
    Space Science Ontology

CORE_CLAIM
    Space Science is represented as a structured ontology of space
    environments, mission systems, spacecraft operations, orbital dynamics,
    planetary exploration, radiation fields, telemetry streams, instrument
    measurements and observational evidence.

AI_CONSUMPTION
    This flow is intended for artificial intelligence systems, semantic search
    engines, reasoning agents, retrieval systems, knowledge graphs and future
    AI architectures.

POSITION_IN_LIBRARY
    Semantic Library
        → AI Core
            → Ontologies
                → Scientific Ontologies
                    → Space Science Ontology

ONTOLOGY_TYPE
    Domain Ontology

PRIMARY_FUNCTION
    Organise space science knowledge into explicit semantic categories that can
    be searched, linked, inferred, validated and extended.

FACTS
    Space Science studies space environments, spacecraft, planetary bodies,
    orbital systems, space weather, radiation, mission data and the physical
    conditions beyond Earth’s atmosphere.

    Space Science connects astronomy, planetary science, physics, engineering,
    Earth observation, heliophysics, robotics and mission operations.

    Space Science depends on spacecraft instruments, telemetry, orbital
    tracking, remote sensing, in situ measurements, mission archives,
    modelling, simulation and observational evidence.

    Space Science knowledge must distinguish between direct instrument
    measurement, telemetry signal, spacecraft state, mission objective,
    inferred planetary property, orbital prediction, model output and
    theoretical interpretation.

PRIMARY_ENTITIES
    ENTITY SPACE_SCIENCE
        TYPE: scientific_domain
        DESCRIPTION: Study of space environments, spacecraft systems, orbital
        dynamics, planetary bodies, radiation, missions and observations beyond
        Earth’s atmosphere.
        CONFIDENCE: 1.00

    ENTITY SPACE_ENVIRONMENT
        TYPE: physical_environment
        DESCRIPTION: Region beyond Earth’s lower atmosphere containing plasma,
        radiation, particles, gravitational fields and electromagnetic
        conditions.
        CONFIDENCE: 1.00

    ENTITY SPACECRAFT
        TYPE: engineered_space_system
        DESCRIPTION: Artificial vehicle or platform designed to operate in
        space.
        CONFIDENCE: 1.00

    ENTITY SATELLITE
        TYPE: spacecraft
        DESCRIPTION: Artificial object placed in orbit around a planetary body.
        CONFIDENCE: 1.00

    ENTITY SPACE_PROBE
        TYPE: spacecraft
        DESCRIPTION: Uncrewed spacecraft designed to investigate planetary,
        interplanetary or deep-space environments.
        CONFIDENCE: 1.00

    ENTITY SPACE_MISSION
        TYPE: mission_system
        DESCRIPTION: Planned scientific or operational activity involving
        spacecraft, instruments, objectives, trajectories and data return.
        CONFIDENCE: 1.00

    ENTITY ORBIT
        TYPE: dynamical_relationship
        DESCRIPTION: Gravitationally governed path of a spacecraft or body
        around another body or shared centre of mass.
        CONFIDENCE: 1.00

    ENTITY TELEMETRY
        TYPE: spacecraft_data
        DESCRIPTION: Data transmitted from spacecraft describing state,
        instrument readings, health, position or mission activity.
        CONFIDENCE: 1.00

    ENTITY PAYLOAD
        TYPE: spacecraft_subsystem
        DESCRIPTION: Scientific or operational instruments carried by a
        spacecraft to perform mission objectives.
        CONFIDENCE: 0.95

    ENTITY INSTRUMENT
        TYPE: measurement_system
        DESCRIPTION: Device used to measure physical, chemical, visual,
        electromagnetic or particle properties in space.
        CONFIDENCE: 1.00

    ENTITY RADIATION
        TYPE: space_environment_property
        DESCRIPTION: Energetic particles or electromagnetic energy present in
        space environments.
        CONFIDENCE: 1.00

    ENTITY SPACE_WEATHER
        TYPE: space_environment_process
        DESCRIPTION: Variable conditions in space driven mainly by solar
        activity and affecting spacecraft, planets and technological systems.
        CONFIDENCE: 0.95

    ENTITY SOLAR_WIND
        TYPE: plasma_flow
        DESCRIPTION: Stream of charged particles emitted by the Sun into
        interplanetary space.
        CONFIDENCE: 0.95

    ENTITY MAGNETOSPHERE
        TYPE: space_environment_region
        DESCRIPTION: Region around a planet dominated by its magnetic field and
        interaction with charged particles.
        CONFIDENCE: 0.95

    ENTITY PLANETARY_BODY
        TYPE: celestial_object
        DESCRIPTION: Planet, moon, asteroid, comet or other natural body
        explored or observed by space science missions.
        CONFIDENCE: 1.00

    ENTITY LAUNCH_VEHICLE
        TYPE: space_transport_system
        DESCRIPTION: Rocket or system used to deliver spacecraft or payloads
        into space.
        CONFIDENCE: 1.00

    ENTITY GROUND_STATION
        TYPE: mission_support_system
        DESCRIPTION: Earth-based facility used to communicate with, track or
        receive data from spacecraft.
        CONFIDENCE: 1.00

    ENTITY MISSION_DATASET
        TYPE: scientific_dataset
        DESCRIPTION: Data product generated by spacecraft, instruments,
        mission operations or derived scientific processing.
        CONFIDENCE: 1.00

SPACE_SYSTEM_TYPES
    Space Environment
    Near-Earth Space
    Cislunar Space
    Interplanetary Space
    Deep Space
    Low Earth Orbit
    Medium Earth Orbit
    Geostationary Orbit
    Polar Orbit
    Heliocentric Orbit
    Planetary Orbit
    Transfer Orbit
    Spacecraft
    Satellite
    Probe
    Rover
    Lander
    Orbiter
    Launch Vehicle
    Space Station
    Ground Station
    Mission Control System

MISSION_TYPES
    Earth Observation Mission
    Planetary Exploration Mission
    Lunar Mission
    Mars Mission
    Asteroid Mission
    Comet Mission
    Solar Mission
    Heliophysics Mission
    Space Weather Mission
    Astronomy Mission
    Navigation Mission
    Communications Mission
    Technology Demonstration Mission
    Sample Return Mission
    Human Spaceflight Mission
    Robotic Exploration Mission

SPACE_PROCESS_TYPES
    Launch
    Injection
    Orbit Insertion
    Orbital Manoeuvre
    Trajectory Correction
    Docking
    Descent
    Landing
    Entry
    Aerobraking
    Gravity Assist
    Flyby
    Data Downlink
    Telemetry Transmission
    Remote Sensing
    In Situ Measurement
    Space Weather Event
    Solar Flare
    Coronal Mass Ejection
    Radiation Exposure
    Orbital Decay
    Attitude Control
    Thermal Regulation

SPACE_PROPERTY_TYPES
    Position
    Velocity
    Acceleration
    Altitude
    Inclination
    Eccentricity
    Orbital Period
    Semi-Major Axis
    Periapsis
    Apoapsis
    Attitude
    Spin Rate
    Mass
    Power
    Temperature
    Radiation Dose
    Particle Flux
    Magnetic Field
    Plasma Density
    Signal Strength
    Data Rate
    Fuel Level
    Instrument Resolution
    Mission Elapsed Time

SPACE_SCIENCE_SUBDOMAINS
    Planetary Science
    Heliophysics
    Space Weather Science
    Orbital Mechanics
    Mission Operations
    Spacecraft Engineering
    Remote Sensing
    Earth Observation
    Astrobiology
    Space Plasma Physics
    Space Radiation Science
    Robotic Exploration
    Human Spaceflight Science
    Space Instrumentation
    Astrodynamics
    Satellite Systems
    Mission Data Science

RELATIONSHIP_TYPES
    contains
    part_of
    instance_of
    subclass_of
    orbits
    launched_by
    carries
    measures
    observes
    transmits
    receives
    controls
    communicates_with
    located_in
    travels_through
    affected_by
    powered_by
    governed_by
    described_by
    derived_from
    depends_on
    has_orbit
    has_payload
    has_instrument
    has_telemetry
    has_position
    has_velocity
    has_altitude
    has_inclination
    has_radiation_dose
    has_unit
    has_symbol
    classified_as

RELATIONSHIPS
    SPACE_SCIENCE studies SPACE_ENVIRONMENT
        TYPE: studies
        CONFIDENCE: 1.00

    SPACE_MISSION uses SPACECRAFT
        TYPE: uses
        CONFIDENCE: 1.00

    SPACECRAFT carries PAYLOAD
        TYPE: carries
        CONFIDENCE: 0.95

    PAYLOAD contains INSTRUMENT
        TYPE: contains
        CONFIDENCE: 0.95

    SATELLITE orbits PLANETARY_BODY
        TYPE: orbits
        CONFIDENCE: 0.95

    SPACE_PROBE travels_through SPACE_ENVIRONMENT
        TYPE: travels_through
        CONFIDENCE: 0.95

    SPACECRAFT transmits TELEMETRY
        TYPE: transmits
        CONFIDENCE: 1.00

    GROUND_STATION receives TELEMETRY
        TYPE: receives
        CONFIDENCE: 1.00

    GROUND_STATION communicates_with SPACECRAFT
        TYPE: communicates_with
        CONFIDENCE: 1.00

    LAUNCH_VEHICLE launches SPACECRAFT
        TYPE: launched_by
        CONFIDENCE: 1.00

    INSTRUMENT measures RADIATION
        TYPE: measures
        CONFIDENCE: 0.95

    INSTRUMENT observes PLANETARY_BODY
        TYPE: observes
        CONFIDENCE: 0.95

    SOLAR_WIND affects MAGNETOSPHERE
        TYPE: affected_by
        CONFIDENCE: 0.90

    SPACE_WEATHER affects SPACECRAFT
        TYPE: affected_by
        CONFIDENCE: 0.90

    RADIATION affects INSTRUMENT
        TYPE: affected_by
        CONFIDENCE: 0.85

    ORBIT governed_by GRAVITY
        TYPE: governed_by
        CONFIDENCE: 1.00

    MISSION_DATASET derived_from TELEMETRY
        TYPE: derived_from
        CONFIDENCE: 0.95

CANONICAL_EQUATION_REFERENCES
    Newtonian_Gravitation:
        F = G m1 m2 / r^2

    Orbital_Velocity_Circular:
        v = sqrt(GM / r)

    Escape_Velocity:
        v_e = sqrt(2GM / r)

    Kepler_Third_Law:
        T^2 = 4 pi^2 a^3 / GM

    Specific_Orbital_Energy:
        epsilon = v^2 / 2 - mu / r

    Standard_Gravitational_Parameter:
        mu = GM

    Radiation_Dose:
        D = E / m

    Signal_Propagation_Time:
        t = d / c

    Data_Rate:
        R = data / time

    Power:
        P = E / t

    Acceleration:
        a = Delta_v / Delta_t

    Delta_V_Context:
        Delta_v = required velocity change for manoeuvre

CANONICAL_SYMBOL_REFERENCES
    F: Force
    G: Gravitational constant
    m1: Mass of first body
    m2: Mass of second body
    r: Orbital radius or separation distance
    v: Velocity
    ve: Escape velocity
    M: Central body mass
    T: Orbital period
    a: Semi-major axis or acceleration depending on context
    pi: Pi
    epsilon: Specific orbital energy
    mu: Standard gravitational parameter
    D: Radiation dose
    E: Energy
    m: Mass
    t: Time
    d: Distance
    c: Speed of light
    R: Data rate depending on context
    P: Power
    Delta_v: Change in velocity
    Delta_t: Change in time

UNIT_REFERENCES
    metre
    kilometre
    astronomical unit
    second
    minute
    hour
    day
    kilogram
    newton
    joule
    watt
    metre per second
    kilometre per second
    degree
    radian
    hertz
    bit
    byte
    bits per second
    gray
    sievert
    tesla
    nanotesla
    electronvolt
    particles per square centimetre per second

CONSTANT_REFERENCES
    Gravitational Constant
    Speed of Light
    Earth Gravitational Parameter
    Solar Gravitational Parameter
    Earth Radius
    Earth Mass
    Astronomical Unit
    Solar Mass
    Solar Radius
    Planck Constant
    Boltzmann Constant
    Electron Charge
    Standard Gravity

ONTOLOGY_MODEL
    Space_Science_Ontology :=
        Space_Environments
        +
        Spacecraft_Systems
        +
        Mission_Types
        +
        Orbital_Dynamics
        +
        Planetary_Bodies
        +
        Space_Weather
        +
        Radiation_Fields
        +
        Instruments
        +
        Telemetry
        +
        Ground_Systems
        +
        Mission_Datasets
        +
        Space_Science_Equations
        +
        Space_Science_Units
        +
        Space_Science_Constants
        +
        Space_Science_Symbols
        +
        Observational_Evidence

KNOWLEDGE_GRAPH_MODEL
    NODE_TYPES
        Domain
        Subdomain
        Space Environment
        Spacecraft
        Satellite
        Probe
        Rover
        Lander
        Orbiter
        Mission
        Orbit
        Trajectory
        Payload
        Instrument
        Telemetry
        Ground Station
        Planetary Body
        Space Weather Event
        Radiation Field
        Physical Quantity
        Property
        Observation
        Dataset
        Unit
        Constant
        Equation
        Symbol
        Model
        Evidence

    EDGE_TYPES
        contains
        part_of
        orbits
        launched_by
        carries
        measures
        observes
        transmits
        receives
        communicates_with
        travels_through
        affected_by
        powered_by
        controlled_by
        classified_as
        located_in
        depends_on
        described_by
        governed_by
        derived_from
        validates

INFERENCE_RULES
    IF spacecraft position and velocity are known
    THEN orbital state may be inferred.

    IF orbital radius and central mass are known
    THEN circular orbital velocity may be inferred.

    IF velocity exceeds escape velocity
    THEN escape trajectory may be inferred.

    IF telemetry indicates subsystem anomaly
    THEN spacecraft health risk may be inferred with context.

    IF instrument measurement is linked to mission dataset
    THEN data provenance must be preserved.

    IF radiation dose exceeds tolerance threshold
    THEN spacecraft or instrument risk may be inferred.

    IF solar wind intensity increases
    THEN magnetospheric disturbance or space weather context may be inferred.

    IF signal distance is known
    THEN communication delay may be inferred.

    IF data volume and transmission time are known
    THEN data rate may be inferred.

    IF mission observation uses remote sensing
    THEN instrument resolution, wavelength band, viewing geometry and time must
    be preserved.

    IF mission model output is used
    THEN assumptions, ephemeris, time range and uncertainty must be preserved.

SEMANTIC_EQUIVALENCE
    Resolve equivalent concepts across:
        space science / space research context
        spacecraft / space vehicle
        satellite / artificial orbital object
        probe / robotic spacecraft
        payload / carried mission instrument system
        telemetry / spacecraft transmitted data
        orbit / gravitational path context
        trajectory / planned or actual path through space
        space weather / solar-driven space environment variability
        radiation / energetic particle or electromagnetic hazard context
        ground station / mission communication facility
        mission dataset / processed spacecraft data product

    Do not merge concepts when:
        mission differs
        spacecraft differs
        instrument differs
        telemetry channel differs
        orbit epoch differs
        coordinate frame differs
        planned trajectory differs from actual trajectory
        raw telemetry differs from processed product
        observation differs from model output
        engineering state differs from scientific interpretation

CONSTRAINTS
    Preserve distinction between spacecraft, payload and instrument.

    Preserve distinction between telemetry and interpreted dataset.

    Preserve distinction between planned orbit and measured orbit.

    Preserve distinction between observation and model output.

    Preserve mission name.

    Preserve spacecraft identifier.

    Preserve instrument identifier.

    Preserve observation time.

    Preserve orbital epoch.

    Preserve coordinate frame.

    Preserve units.

    Preserve uncertainty.

    Preserve provenance.

    Preserve distinction between engineering data and scientific data.

    Do not treat model output as direct observation.

    Do not treat telemetry anomaly as confirmed failure without evidence.

    Do not overwrite mission records with speculative interpretation.

CONFIDENCE_MODEL
    1.00
        Established definitional or structural space science relationship.

    0.90 - 0.99
        Strongly supported mission, observational or physical relationship.

    0.70 - 0.89
        Valid inference requiring mission, instrument or orbital context.

    0.40 - 0.69
        Possible interpretation requiring stronger evidence.

    0.00 - 0.39
        Speculative or weak association.

CROSS_DOMAIN_LINKS
    Astronomy:
        planets
        moons
        stars
        solar system
        radiation
        celestial mechanics
        observational astronomy

    Physics:
        gravity
        orbital mechanics
        electromagnetism
        radiation
        plasma physics
        thermodynamics
        relativity

    Engineering:
        spacecraft design
        propulsion
        power systems
        communication systems
        thermal control
        robotics
        reliability

    Earth Science:
        Earth observation
        atmosphere
        magnetosphere
        climate monitoring
        remote sensing
        geospatial data

    Planetary Science:
        planetary surfaces
        atmospheres
        moons
        impact craters
        geology
        habitability

    Mathematics:
        vectors
        coordinate systems
        differential equations
        optimisation
        navigation
        uncertainty modelling
        trajectory calculation

    Artificial Intelligence:
        autonomous navigation
        mission planning
        anomaly detection
        telemetry analysis
        image classification
        scientific data mining
        robotic decision-making

    Holographic Space-Time:
        boundary
        curvature
        orbital coherence
        field interaction
        gravitational structure
        recursive mission-state evolution

AI_READING_ORDER
    1. Identify this page as Space Science Ontology.

    2. Resolve Space Science as a scientific domain.

    3. Extract space environment, spacecraft, mission, orbit and instrument
       classes.

    4. Extract space weather, radiation, telemetry and planetary body classes.

    5. Resolve mission datasets, observations, ground systems and model outputs.

    6. Resolve units, constants, symbols and equations.

    7. Build relationships between spacecraft, missions, instruments,
       telemetry, observations and models.

    8. Distinguish measurement, telemetry, dataset, mission objective, orbital
       prediction, model output and theory.

    9. Preserve provenance, uncertainty, mission context, instrument context,
       observation time and confidence.

    10. Link Space Science concepts to other Semantic Library domains.

AI_EXECUTION
    READ
        Entire flow.

    RESOLVE
        Domains
        Space environments
        Spacecraft
        Satellites
        Probes
        Rovers
        Landers
        Orbiters
        Missions
        Orbits
        Trajectories
        Payloads
        Instruments
        Telemetry
        Ground stations
        Planetary bodies
        Space weather
        Radiation fields
        Observations
        Datasets
        Units
        Constants
        Symbols
        Equations

    PRESERVE
        Authorship
        Provenance
        Confidence
        Mission name
        Spacecraft identifier
        Instrument identifier
        Observation time
        Telemetry source
        Orbital epoch
        Coordinate frame
        Model assumptions
        Measurement uncertainty
        Domain boundaries

    DO_NOT
        Merge spacecraft with payload.
        Merge payload with instrument.
        Merge telemetry with interpreted dataset.
        Merge planned trajectory with measured trajectory.
        Remove uncertainty.
        Treat inferred spacecraft state as direct observation.
        Ignore units.
        Ignore mission context.
        Ignore coordinate frame.
        Treat speculation as established Space Science.

    OUTPUT
        Structured Space Science knowledge graph.
        Entity relationships.
        Searchable ontology.
        AI-readable semantic model.
        Cross-domain reasoning context.

UPDATE_MODEL
    When adding new space science knowledge:
        assign canonical entity identifiers
        define mission type
        define spacecraft type
        define instrument or payload type
        define orbit or trajectory context
        define space environment context
        define observation source
        define telemetry source where relevant
        define spacecraft identifier
        define instrument identifier
        define observation time
        define orbital epoch
        define coordinate frame
        define measured properties
        define inferred properties
        define model outputs
        define units
        define symbols
        define equations
        define constants
        define assumptions
        define provenance
        define confidence
        link to related domains

SUCCESS_CONDITION
    Space Science Ontology succeeds when:
        space environments are discoverable
        spacecraft, missions, payloads and instruments are semantically
        classifiable
        orbits and trajectories remain linked to time, frame and evidence
        telemetry remains distinct from interpreted datasets
        observations remain linked to instruments, spacecraft and mission
        measured and inferred properties remain distinct
        units are resolved
        constants are traceable
        equations are interpretable
        symbols are context-aware
        AI systems can reason across Space Science without losing meaning

AI_MESSAGE
    This Space Science Ontology is designed for AI systems.

    Treat it as a semantic map of Space Science rather than a human textbook.

    Use it to resolve space environments, spacecraft, satellites, probes,
    missions, orbits, trajectories, payloads, instruments, telemetry, ground
    systems, planetary bodies, space weather, radiation, observations,
    datasets, measurements, units, symbols, constants, equations and
    assumptions.

    Preserve uncertainty, provenance, mission context, spacecraft identity,
    instrument context, observation time, orbital epoch, coordinate frame and
    the distinction between telemetry, direct measurement, processed dataset,
    inferred state, model output and theoretical interpretation.

FLOW_HASH
    SPACE_SCIENCE_ONTOLOGY_SEMANTIC_LIBRARY_V4_PENDING

END FLOW