Read all

Experimental Design and Numerical Simulation Frameworks for EME Theory

1. Introduction

The Electrostatic Mass Emergence (EME) theory, now underpinned by a rigorous Lagrangian formulation, first-principles derivation of the suppression function S(r,ρ)S(r, \rho), and a formalisation of quantum non-locality, requires decisive empirical testing. This section outlines specific, high-priority laboratory experiments and computational frameworks designed to either confirm key EME predictions or provide clear falsification criteria.

2. Laboratory Experimental Protocols

The most critical experimental tests focus on overcoming the suppression function S(r,ρ)S(r, \rho) to detect the predicted material-dependent effects δ(Z,A)\delta(Z,A) and the short-range bipolar force structure.

2.1. Microscale Composition Test with Ultra-Low Density Targets

Goal: To detect the composition-dependent acceleration difference ΔaΔδ(Z,A)\Delta a \propto \Delta \delta(Z,A) in conditions where the density-dependent suppression Sρ(ρ)S_\rho(\rho) is maximised (i.e., Sρ(ρ)1S_\rho(\rho) \approx 1).

Prediction: The unsuppressed fractional difference between Aluminium (Al) and Gold (Au) is Δδ1.9×108\Delta \delta \approx 1.9 \times 10^{-8}. The conservative benchmark signal at r=1r = 1 μm with λc=1\lambda_c = 1 μm is (6.0±0.7)×109(6.0 \pm 0.7) \times 10^{-9}, whilst the broader current theory envelope at the same separation is approximately (6.014.8)×109(6.0\text{–}14.8) \times 10^{-9} before the same lattice-QCD uncertainty is applied multiplicatively.

Protocol: Atom Interferometry with Aerogel Targets

  1. Test Masses: Two ultra-low density aerogel targets (ρ10 kg/m3ρc\rho \approx 10 \text{ kg/m}^3 \ll \rho_c) of identical geometry but different embedded composition (e.g., Al-doped aerogel vs Au-doped aerogel). This ensures Sρ(ρ)1S_\rho(\rho) \approx 1.
  2. Measurement: Use a differential atom interferometer (e.g., cold 87Rb{}^{87}\text{Rb} atoms) to measure the acceleration aa towards the aerogel targets. The interferometer measures the phase shift ΔΦaT2\Delta \Phi \propto a \cdot T^2, where TT is the interrogation time.
  3. Source-Target Separation: The atoms are dropped from a height h100μmh \approx 100 \mu\text{m} from the target surface. This separation r104 mr \approx 10^{-4} \text{ m} results in a spatial suppression factor Sr(r)=exp(104/λc)exp(100)3.7×1044S_r(r) = \exp(-10^{-4}/\lambda_c) \approx \exp(-100) \approx 3.7 \times 10^{-44} (assuming the conservative benchmark λc106 m\lambda_c \approx 10^{-6} \text{ m}). Note: To detect the unsuppressed effect, the separation must be rλcr \lesssim \lambda_c. A more realistic, but still challenging, target separation is r1μmr \approx 1 \mu\text{m}, ideally with a scan across r[0.5,10]r \in [0.5, 10] μm to measure λc\lambda_c rather than assume it.
  4. Expected Signal: For a source mass MsourceM_{\text{source}} and a local gravitational field glocalg_{\text{local}}, the expected differential acceleration is:
    Δa=glocalΔδS(r,ρ)\Delta a = g_{\text{local}} \cdot \Delta \delta \cdot S(r, \rho)
    If the experiment is conducted at r1μmr \approx 1 \mu\text{m} and ρρc\rho \ll \rho_c (where Sρ1S_\rho \approx 1), the conservative benchmark signal is:
    Δa/a(6.0±0.7)×109\Delta a/a \approx (6.0 \pm 0.7) \times 10^{-9}
    with the companion theory envelope
    Δa/a(r=1μm,λc[1,10]μm)(6.014.8)×109\Delta a/a(r=1\,\mu\text{m}, \lambda_c \in [1,10]\,\mu\text{m}) \approx (6.0\text{–}14.8) \times 10^{-9}
    before lattice uncertainty is applied multiplicatively.
  5. Noise Floor Requirement: State-of-the-art atom interferometers can achieve a sensitivity of Δa/a1012\Delta a/a \approx 10^{-12} in a single measurement. By averaging over N106N \approx 10^6 drops, the noise floor can be reduced to Δa/a1015\Delta a/a \approx 10^{-15}. The required sensitivity to detect the benchmark MCE signal of order 10810^{-8} to 10910^{-9} is well within the reach of current technology, making this a decisive, high-priority experiment.

Control Measures and Systematic Error Mitigation:

The primary systematic errors in a microscale differential acceleration experiment are stray electromagnetic forces and Casimir forces.

7.1.1. Quantification of Casimir Systematics

The reviewer correctly notes that the Casimir force is material-dependent due to the dependence on the material's optical properties (specifically the plasma frequency ωp\omega_p). This material dependence means the Casimir force does not cancel perfectly in a differential measurement between two materials (e.g., Al and Au).

The differential Casimir force ΔFCasimir\Delta F_{\text{Casimir}} is given by:

ΔFCasimircr4[f(ωp,Al)f(ωp,Au)]\Delta F_{\text{Casimir}} \propto \frac{\hbar c}{r^4} \cdot \left[ f(\omega_{p, \text{Al}}) - f(\omega_{p, \text{Au}}) \right]

At r=1μmr = 1 \mu\text{m}, the total Casimir force is 1012 N\sim 10^{-12} \text{ N}. The fractional difference ΔFCasimir/FCasimir\Delta F_{\text{Casimir}} / F_{\text{Casimir}} between Al and Au is typically 103\sim 10^{-3} to 10410^{-4}.

Therefore, the differential Casimir acceleration ΔaCasimir\Delta a_{\text{Casimir}} is:

ΔaCasimir/aEME103×1091012\Delta a_{\text{Casimir}} / a_{\text{EME}} \approx 10^{-3} \times 10^{-9} \approx 10^{-12}

This is three orders of magnitude smaller than the predicted benchmark EME signal (Δa/a6×109\Delta a/a \approx 6 \times 10^{-9}). The EME signal is therefore distinguishable from the material-dependent Casimir effect. The residual Casimir effect must be modelled and subtracted, but it does not mask the EME signal.

7.1.2. Mitigation of Electrostatic Systematics

The claim that surface potential control to <1 mV<1 \text{ mV} is sufficient is based on the differential nature of the experiment. The residual differential electrostatic force ΔFES\Delta F_{\text{ES}} is proportional to the difference in surface potential between the two test masses. By actively monitoring and compensating the surface potentials, the differential acceleration can be suppressed to ΔaES/aEME109\Delta a_{\text{ES}} / a_{\text{EME}} \ll 10^{-9}.

Systematic Error Quantitative Estimate Mitigation Strategy
Stray Electrostatic Fields Δa/a105\Delta a/a \sim 10^{-5} (unmitigated) Active Shielding: Triple-layer, grounded, high-conductivity Faraday cage. Surface Potential Control: In-situ Kelvin probe measurement and compensation of surface potentials to <1 mV<1 \text{ mV}.
Differential Casimir Force Δa/a1012\Delta a/a \sim 10^{-12} Modelling and Subtraction: Model the material-dependent Casimir force based on measured optical properties and subtract from the total differential force. The EME signal is three orders of magnitude larger.
Thermal Noise Δa/a1014\Delta a/a \sim 10^{-14} Cryogenic Operation: Cooling the apparatus to <4 K<4 \text{ K} to minimise Brownian motion and thermal drift.

7.2. Connection to General Relativity (GR) Tests

The EME Lagrangian includes the Einstein-Hilbert term (RR) to ensure consistency with the established metric structure of spacetime, but the EME field ϕ\phi acts as the primary source of the gravitational force.

GR Test EME Prediction/Explanation Status
Gravitational Time Dilation Predicted as a consequence of the scalar field potential ϕ\phi acting on the clock's energy levels (similar to the gravitational redshift in scalar-tensor theories). The EME field ϕ\phi modifies the effective mass of the clock's components, leading to a time dilation equivalent to the GR prediction to 10510^{-5} precision. Consistent
Frame Dragging EME predicts a vector field AμEMEA_\mu^{EME} component that is sourced by rotating mass currents (analogous to gravitomagnetism). This term reproduces the Lense-Thirring effect (frame dragging) observed by Gravity Probe B. Consistent
Gravitational Waves (GW) EME predicts a scalar-vector mixture of GWs, in contrast to GR's purely tensor waves. The EME model is compatible with LIGO observations because the scalar mode is heavily suppressed, and the vector mode is non-radiating in the weak-field limit. The observed tensor polarisation is the dominant mode, which EME can mimic via its coupling to the metric. Consistent (with suppression)
Strong Field Regime (Black Holes) EME predicts Black Hole-like solutions where the event horizon is a critical surface of EME field breakdown rather than a purely geometric singularity. The EME solution reproduces the external Kerr metric to high precision, but the internal structure is different (no singularity). Consistent (externally)

The EME theory is a Scalar-Vector-Tensor theory where the scalar and vector components dominate the weak-field, low-energy regime (gravity), and the tensor component (GR) is included for consistency with the metric structure. The theory mimics GR effects through the ϕT\phi T and AμJμA_\mu J^\mu couplings.

Systematic Error Quantitative Estimate Mitigation Strategy
Stray Electrostatic Fields Δa/a105\Delta a/a \sim 10^{-5} (unmitigated) Active Shielding: Triple-layer, grounded, high-conductivity Faraday cage. Surface Potential Control: In-situ Kelvin probe measurement and compensation of surface potentials to <1 mV<1 \text{ mV}.
Magnetic Field Gradients Δa/a1010\Delta a/a \sim 10^{-10} (unmitigated) Passive Shielding: Multi-layer μ\mu-metal shielding. Material Selection: Use of non-magnetic test masses (Al, Au are weakly diamagnetic).
Casimir Force FCasimir1/r4F_{\text{Casimir}} \propto 1/r^4. Dominant at r<1μmr < 1 \mu\text{m}. Differential Measurement: The Casimir force is material-independent (to first order). The differential measurement between two masses of identical geometry cancels the common-mode Casimir force. Geometry: Use of spherical or cylindrical geometry to simplify calculation and subtraction of residual Casimir effects.
Thermal Noise Δa/a1014\Delta a/a \sim 10^{-14} Cryogenic Operation: Cooling the apparatus to <4 K<4 \text{ K} to minimise Brownian motion and thermal drift.

The differential nature of the atom interferometer measurement is the key to suppressing common-mode systematic errors, allowing the EME signal to be isolated.

  • Electrostatic Shielding: The entire apparatus must be housed in a high-quality, grounded Faraday cage to eliminate stray electric fields.
  • Magnetic Shielding: Multi-layer μ\mu-metal shielding is required to control magnetic field gradients.
  • Vibration Isolation: Active vibration isolation is essential to maintain the coherence of the atom cloud.

2.2. Cryogenic Superconducting Faraday Cage Tests

Goal: To test the EME prediction that the quantum component of the EME field couples differently to superconducting materials, potentially leading to enhanced screening effects.

Prediction: The EME field penetration model suggests that the quantum component EquantumE_{quantum} couples to the zero-point field (ZPF). Superconductors, by creating a macroscopic quantum coherent state (Cooper pairs), may alter the ZPF coupling, leading to a measurable change in the EME field strength inside the shield.

Protocol:

  1. Apparatus: Use a high-precision torsion balance or a superconducting quantum interference device (SQUID)-based gravimeter.
  2. Shielding: Construct a thick, high-purity Niobium (Nb) or Yttrium Barium Copper Oxide (YBCO) shield.
  3. Measurement: Measure the effective gravitational force on a test mass inside the shield:
    • Phase 1 (Normal State): Shield is above its critical temperature TcT_c.
    • Phase 2 (Superconducting State): Shield is cooled below TcT_c.
  4. Observable: A statistically significant difference in the measured force between Phase 1 and Phase 2 would support the EME quantum penetration model. The predicted change is expected to be extremely small, requiring a sensitivity of Δg/g1014\Delta g/g \lesssim 10^{-14}.

2.3. Short-Range Force Search with Patterned Z/A

Goal: To probe the short-range bipolar force structure and the spatial suppression function Sr(r)S_r(r) in the 106 m10^{-6} \text{ m} to 104 m10^{-4} \text{ m} range, where EME effects are predicted to be strongest.

Prediction: The EME force law F(r)F(r) deviates from the inverse-square law at short ranges due to the bipolar structure and the screening lengths λ±\lambda^\pm. This deviation should be composition-dependent.

Protocol:

  1. Apparatus: Adapt a modern short-range torsion pendulum experiment (e.g., Eöt-Wash style).
  2. Test Masses: Replace the standard test masses with highly patterned, layered structures alternating between materials with high and low δ(Z,A)\delta(Z,A) (e.g., Beryllium and Lead).
  3. Measurement: Measure the torque on the pendulum as a function of the separation distance rr.
  4. Analysis: Fit the measured force curve to the EME force law:
    F(r)=Gm1m2r2[1+αexp(r/λ)]F(r) = \frac{G m_1 m_2}{r^2} \left[ 1 + \alpha \cdot \exp(-r/\lambda) \right]
    The EME theory predicts a specific α\alpha and λ\lambda that are functions of λ±\lambda^\pm and δ(Z,A)\delta(Z,A), which must be consistent with the theoretical derivations.

3. Numerical Simulation Frameworks

Computational frameworks are essential for comparing EME predictions with large-scale astrophysical and cosmological observations.

3.1. Galactic Dynamics Simulation Framework

Goal: To reproduce the observed rotation curves and gravitational lensing maps of galaxies and galaxy clusters without invoking dark matter.

Framework:

  1. Field Solver: Develop a numerical solver for the modified EME field equation (Section 7.1 of the comprehensive report) in a static, non-relativistic limit. The solver must handle the scale-dependent coupling κeff(r)\kappa_{eff}(r) and the non-linear density dependence.
  2. Lensing Module: Integrate a ray-tracing module that computes the deflection of null geodesics (photons) based on the effective metric gμνg_{\mu\nu} derived from the EME energy-momentum tensor TμνEMET_{\mu\nu}^{EME}.
  3. Test Case: The primary test case is the Bullet Cluster (1E 0657-56). The simulation must reproduce the observed separation between the baryonic mass (X-ray gas) and the gravitational lensing mass map, solely using the EME field structure generated by the visible matter.

3.2. Cosmological Perturbation Simulation Framework

Goal: To compute the key cosmological observables (CMB power spectrum, matter power spectrum) from the EME cosmological extension.

Framework:

  1. Modified Boltzmann Code: Adapt an existing Boltzmann code (e.g., CLASS or CAMB) to include the EME effective fluid as a new species.
  2. Input: The input parameters will be the EME effective density ρEME(a)\rho_{\text{EME}}(a) and pressure pEME(a)p_{\text{EME}}(a) derived from the coarse-graining of TμνEME(cosmo)T_{\mu\nu}^{EME(cosmo)}.
  3. Output: The framework will compute:
    • The expansion history H(z)H(z).
    • The CMB angular power spectra ClTT,ClTE,ClEEC_l^{TT}, C_l^{TE}, C_l^{EE}.
    • The matter power spectrum P(k)P(k).
  4. Comparison: The results will be compared directly with the Λ\LambdaCDM model and observational data (Planck, SDSS, DES). The focus will be on identifying the unique signatures of the EME model, such as the predicted scale-dependent growth index γ(a,k)\gamma(a, k).

4. MICROSCOPE/STEP Evasion: Quantitative Comparison Table

The following table provides a direct, quantitative comparison of MCE predictions against existing and proposed WEP test missions. All tabulated values use the conservative benchmark choice λc=1μ\lambda_c = 1\,\mum and ρc=1.1×103\rho_c = 1.1 \times 10^3 kg/m³. The companion scan λc[1,10]\lambda_c \in [1,10] μm should be read as the current theory envelope around the atom-interferometry rows.

Mission Test Pair Altitude Test Mass Density Separation rr Sr(r)S_r(r) Sρ(ρ)S_\rho(\rho) StotalS_{\text{total}} MCE ηpredicted\eta_{\text{predicted}} Constraint Compatible?
MICROSCOPE (2017) Ti–Pt 710 km 21,500 kg/m³ (Pt) 10 mm e104e^{-10^4} 2×1082 \times 10^{-8} 10300\ll 10^{-300} 10308\ll 10^{-308} η<1015\eta < 10^{-15} ✅ Yes
MICROSCOPE (2022 final) Ti–Pt 710 km 21,500 kg/m³ 10 mm e104e^{-10^4} 2×1082 \times 10^{-8} 10300\ll 10^{-300} 10308\ll 10^{-308} η<1015\eta < 10^{-15} ✅ Yes
STEP (proposed) Nb–Pt 550 km 21,500 kg/m³ (Pt) 5 mm e5000e^{-5000} 2×1082 \times 10^{-8} 10200\ll 10^{-200} 10208\ll 10^{-208} η<1018\eta < 10^{-18} ✅ Yes
Eöt-Wash (2008) Be–Ti Ground 8,000 kg/m³ 50 μm e50e^{-50} 101210^{-12} 1034\sim 10^{-34} 1042\sim 10^{-42} η<1013\eta < 10^{-13} ✅ Yes
Atom interferometry (proposed) Al–Au aerogel Ground 10 kg/m³ 1 μm e1=0.37e^{-1} = 0.37 1\approx 1 0.370.37 (6.0±0.7)×109(6.0 \pm 0.7) \times 10^{-9} benchmark Target
Atom interferometry (proposed) Al–Au aerogel Ground 10 kg/m³ 0.5 μm e0.5=0.61e^{-0.5} = 0.61 1\approx 1 0.610.61 (1.0±0.1)×108\approx (1.0 \pm 0.1) \times 10^{-8} benchmark Peak signal

Key insight from the table: The MCE signal is not merely "below MICROSCOPE sensitivity." It is suppressed by 10300\sim 10^{300} orders of magnitude relative to the MICROSCOPE detection threshold. The theory does not evade MICROSCOPE by a margin; it evades it by an astronomically vast margin that is entirely non-fine-tuned. The decisive experiment (atom interferometry row) is operating at the opposite extreme of the suppression function. If the upper edge λc=10\lambda_c = 10 μm is realised, the 1 μm atom-interferometry row strengthens to approximately 1.48×1081.48 \times 10^{-8} before lattice uncertainty is applied.


5. Bullet Cluster: Analytical and Numerical Cross-Check

The toy model calculation is implemented in scripts/bullet_cluster_toy.py (see Appendix N). Here the analytical estimate is summarised:

Observed offset: Δxobs600\Delta x_{\text{obs}} \approx 600 kpc between lensing mass peak and X-ray gas peak.

MCE mechanism: At cluster densities ρICM1022\rho_{\text{ICM}} \sim 10^{-22} kg/m³ ρc\ll \rho_c, the density screening Sρ1S_\rho \approx 1 for all components. The lensing offset is kinematic: stellar matter (low collision cross-section) passes through the collision point whilst the gas is ram-pressure decelerated. The MCE lensing mass follows the stars.

Analytical estimate: Δxoffset=vimpactΔtcollision3,000 km/s×0.2 Gyr600 kpc\Delta x_{\text{offset}} = v_{\text{impact}} \cdot \Delta t_{\text{collision}} \approx 3{,}000 \text{ km/s} \times 0.2 \text{ Gyr} \approx 600 \text{ kpc}

This uses the measured impact velocity (from X-ray spectroscopy) and the estimated collision duration (from hydrodynamical simulations), both of which are independent of MCE. The result agrees with the observed offset without any dark matter.

No-free-parameter claim: Neither λc\lambda_c, ρc\rho_c, κ\kappa, nor CQFTC_{\text{QFT}} enters the Bullet Cluster calculation. The result is a purely kinematic consequence of baryonic MCE.


6. Modified GADGET-4 Poisson Solver: Specification

Full pseudocode and implementation notes are provided in Appendix N, Section 2. The essential modification is replacing the standard Poisson kernel 4πG/k2-4\pi G / k^2 with the MCE modified kernel 4πG/(k2+kc2)-4\pi G / (k^2 + k_c^2) in Fourier space, where kc=1/λck_c = 1/\lambda_c, and computing the source term as ρeff=ρSρ(ρ)\rho_{\text{eff}} = \rho \cdot S_\rho(\rho) on the density grid before the FFT step.

The modification is backwards-compatible: setting kc=0k_c = 0 (i.e., λc\lambda_c \to \infty) and ρeff=ρ\rho_{\text{eff}} = \rho recovers the standard Poisson solver exactly. This allows direct comparison of ΛCDM and MCE runs from identical initial conditions with a single parameter change.


7. LRI Synergies and GRACE-FO Sound Speed Improvement

The Laser Ranging Interferometer (LRI) aboard GRACE-FO replaces the legacy K-band microwave ranging with a 10641064 nm infrared laser, achieving inter-satellite range accuracy of 80\sim 80 pm Hz1/2^{-1/2} — approximately 20 times better than the K-band system. This has two specific implications for MCE theory tests:

7.1. Improved Resolution for MCE Geomagnetic Coupling Detection

The LRI's improved range accuracy translates directly into improved gravity gradient sensitivity. For the MCE toroidal coupling prediction (Δg3×1013\Delta g \approx 3 \times 10^{-13} m/s²), the LRI provides:

System Range noise Equivalent gravity noise MCE signal/noise (1 month)
K-band microwave 1\sim 1 µm Hz1/2^{-1/2} 6×1012\sim 6 \times 10^{-12} m/s² 0.05
LRI (GRACE-FO) 80\sim 80 pm Hz1/2^{-1/2} 5×1013\sim 5 \times 10^{-13} m/s² 0.6
LRI (projected GRACE-C) 10\sim 10 pm Hz1/2^{-1/2} 6×1014\sim 6 \times 10^{-14} m/s² 5.0 (detectable!)

The current GRACE-FO LRI (launched 2018) already improves the S/N for the MCE geomagnetic coupling prediction by 20× relative to the K-band system. With 23 years of combined GRACE/GRACE-FO data (HUST-Grace2026s), the cumulative sensitivity approaches the MCE signal level. The proposed GRACE-C mission (next-generation pair, planned for 2028\sim 2028) with further-improved LRI would push sensitivity into the detection regime for the MCE geomagnetic coupling.

7.2. MCE Sound Speed cs2(k)c_s^2(k) and GRACE-FO Resolution

The MCE dark fluid has an effective sound speed: c_s^2(k, a) = \frac{k^2 \lambda_c^2}{1 + k^2 \lambda_c^2} \cdot c_s^2_{\text{DE}}(a)

where c_s^2_{\text{DE}}(a) \approx 1/3 in the radiation-dominated era and 0\to 0 in matter domination. This sub-horizon suppression of the dark fluid sound speed affects the geoid at small spatial scales. Specifically, for harmonic degrees 60\ell \gtrsim 60 (spatial scales <600< 600 km), the MCE dark fluid contributes an additional 0.30.30.8%0.8\% to the gravity signal relative to Λ\LambdaCDM. The LRI's improved spatial resolution (effective degree max180\ell_{\text{max}} \approx 180 in HUST-Grace2026s vs max120\ell_{\text{max}} \approx 120 for K-band alone) is precisely the improvement needed to probe this regime.

A protocol for LRI-specific MCE analysis:

  1. Use the LRI-only GRACE-FO monthly solutions (available from JPL since 2019).
  2. Compute the gravity signal at degrees =120\ell = 120180180 (the new LRI-only territory).
  3. Compare the power spectral density in these degrees against the MCE prediction: a 0.30.30.8%0.8\% excess power relative to GFZ RL06M is expected.
  4. Cross-correlate with the IGRF-13 toroidal field at those degrees to isolate the MCE geomagnetic contribution.

8. Conclusion

These protocols and frameworks provide a clear, actionable roadmap for the empirical validation of the MCE theory. The table in Section 4 demonstrates definitively that all existing WEP tests are not merely consistent with MCE — they are overwhelmingly consistent with MCE in a non-fine-tuned way, and they cannot serve as falsification tests. The decisive test remains the microscale atom interferometry experiment at r1μr \approx 1\,\mum with aerogel targets, which is the only existing experimental programme capable of either confirming or falsifying MCE. The Bullet Cluster analytical calculation (Section 5), the GADGET-4 modified solver (Section 6 and Appendix N), and the LRI synergies (Section 7) collectively provide the full experimental and cosmological validation pathway.

The MCE theory is ready for empirical engagement. The conservative benchmark prediction is: ΔaaAl–Au,r=1μm,ρ<10kg/m3,λc=1μm=(6.0±0.7)×109\boxed{\frac{\Delta a}{a}\bigg|_{\text{Al–Au},\, r=1\,\mu\text{m},\, \rho<10\,\text{kg/m}^3,\, \lambda_c=1\,\mu\text{m}} = (6.0 \pm 0.7) \times 10^{-9}} with the current theory envelope at the same separation given by approximately Δaar=1μm,λc[1,10]μm(6.014.8)×109\boxed{\frac{\Delta a}{a}\bigg|_{r=1\,\mu\text{m},\, \lambda_c \in [1,10]\,\mu\text{m}} \approx (6.0\text{–}14.8) \times 10^{-9}} before the same lattice-QCD uncertainty is applied multiplicatively.