Artemis campaign

Moon to Mars architecture.

Artemis ties SLS, Orion, Gateway, human landing systems, spacesuits, surface power, science, and international partnerships into a sustained lunar exploration campaign.

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Architecture

Major Artemis systems

SLS

Exploration-class super heavy-lift launch vehicle for Orion and large lunar payloads.

Orion

Crew spacecraft for launch, deep-space transit, reentry, and crew survival.

Gateway

Lunar-orbit platform for staging, science, logistics, and international collaboration.

Human Landing System

Transfers crew between lunar orbit and the surface; large reusable lander concepts are part of current planning.

Surface Systems

Spacesuits, habitats, mobility, communications, power, navigation, and science payloads.

Mars Preparation

The Moon provides an operational testbed for long-duration human exploration farther out.

Artemis I

Uncrewed SLS/Orion flight test demonstrated the integrated system.

Artemis II

Crewed lunar flyby test validates human operations beyond low Earth orbit.

Artemis III+

Surface missions target lunar south-pole science and increasingly capable infrastructure.

Mathematical model

Engineering geometry model

Engineering models are procedural, dimensionally organized teaching models. They use geometric primitives, known subsystem layout, symmetry, and transformation matrices; they are not generated from a visual image and are not exact manufacturing CAD.

Rigid transform

\[\mathbf{p}_{\mathrm{world}}=TRS\,\mathbf{p}_{\mathrm{local}}\]

Every component is positioned by translation T, rotation R, and scale S. This gives a reproducible mathematical scene graph instead of freehand drawing.

Symmetry and repetition

\[\mathbf{p}_k=R_z\!\left(\frac{2\pi k}{N}\right)\mathbf{p}_0\]

Repeated structures such as solar panels, trusses, engines, wheels, and array segments are generated by rotational or translational symmetry.

Scale verification

\[\mathrm{ratio}_{\mathrm{scene}}=\frac{\mathrm{dimension}_a}{\mathrm{dimension}_b}\]

Where the page presents relative component sizes, the scene preserves those ratios or states when readability scaling is applied.

Verification standard: the rendered object must be reproducible from stated equations, catalog parameters, or explicit geometric transforms. Visual reference images may inform presentation only; they are not the source of orbital positions, field vectors, accretion-disk gradients, timing, or engineering layout.

Limitations: browser scenes may use bounded scale, compressed distances, simplified two-body dynamics, schematic transfer curves, or educational approximations where full numerical ephemerides, CFD, finite-element models, or general-relativistic ray tracing are outside the page scope. Those simplifications are part of the model contract, not hidden image-based construction.

Open the full site-wide mathematical verification policy