See the forces.
Follow the energy.

Surface adhesion: a static floor, wall or ceiling check, with a 10 s battery run. The required reaction is N = Fₛ + mg cos θ and the grip reserve is μ max(0, N) − |mg sin θ|. A failed check shows an unsupported pose, not a prediction that the car remains attached.

Vertical lift: thrust and gravity determine height; the mass decreases as air leaves. The run is displayed through the first sampled return to the ground plane. It does not predict body impact, suspension travel or a safe landing.

Airborne roll: the lift burn ends before two balanced roll-jet pulses. Each couple has zero net translational force; τ / I drives angular speed and angle. Both opposed jets consume air at 2|τ| / (d vₑ). Constant roll inertia and unchanged tank pressure are assumptions. This is one-axis rotation, not a six-degree-of-freedom vehicle model.

Tank refill: the compressor draws power until the tank is full or the chosen time expires. The stated isothermal estimate is w = R T ln(p₂/p₁) / η. Flow equals P / w; this is a study operating point, not a compressor map.

The cell choices and pack mass come from Lemonergy’s pinned Designer / Garage parts snapshot. Each cell retains its source basis and estimated fields. Candidate S/P layout is editable and is not a claimed Roadster configuration.

The pack uses constant nominal open-circuit voltage U and series resistance R. I = 2P / [U + √(U² − 4RP)], V = U − IR, heat = I²R, and dSOC/dt = −I/(3600 Q). Negative U² − 4RP flags infeasible electrical demand. Cell continuous current, contactor/fuse carry current and the 5% study SOC floor are checked; pulse capability is not assumed.

Fan pressure and power scale with command squared and cubed. The seal is ideal and fixed hardware does not become stronger when a heavier pack is selected. No OCV–SOC curve, temperature dependence, RC polarization, pressure blow-down, leakage, cooling system, aging, BMS or structural limit is solved. Beyond a rating flag, the trace describes hypothetical demand.

Public nominal ratings do not independently validate these vehicle scenarios. Thrust, inertia, fan operating point, timing, body/rig mass and compressor inputs are editable authored assumptions.

Use the guided block builder above, then run the assembled graph. Download the block-by-block recipe for every parameter, wire, solver setting and reference result. Reopen the native model in this lab to rerun it, or import it into Simulation Studio with catalog 2026.10.1 and the required blocks. The model includes its input assumptions, component provenance and engine hash. CSV contains the displayed native samples; the run record includes the graph, solver identity and validity flags.

• NASA Glenn: thrust and equivalent exhaust velocity
• OpenStax: static friction and normal load
• OpenStax: torque and rotational inertia
• Pinned Lemonergy cell, component and mass records
• Page source & tests (AGPL; asset licences included) · Native graph author · Existing engine corresponding source
• User-supplied visual reference · Tesla demonstration reference

The illustration is not CAD; representative cells, tank volume and nozzle positions are schematic. Force arrows use a fixed scale with a display cap, while numeric values remain uncapped.