MF-01 / Preliminary apparatus plan

Build toward
one defensible result.

A concrete first architecture for optical-force metrology: geometry, calibration, uncertainty allocations, controls and acceptance gates.

Preliminary architecture · not purchase-ready. These dimensions and tolerances are proposed engineering requirements. No force balance, vacuum system or laser has been procured or qualified.
CHAMBER + THERMAL SHIELDEXTERNALLASERPICKOFFBEAM DUMPFORCE →SEPARATEANGLE READOUTSUSPENSIONCOUNTERWEIGHTElectrode calibration · temperature · pressureNormal-incidence reference; outgoing path offset for legibility. Not to scale.
Conceptual geometry, not a fabrication drawing. Force is perpendicular to the balance arm. Source, optical pickoff, dump and detector remain off the suspended assembly.

Freeze one observable

The initial measurement is the full beam-on minus beam-off force on a passive mirror. The external beam is normal to the ideal mirror; its force is perpendicular to a 0.10 m balance arm. At 1 W intercepted power, ideal F = 2P/c = 6.671 nN. Actual reflection, transmission, scatter, alignment and absorption must be measured. This is a new commissioning design point, separate from the earlier 10 W / 80% / ±30° lateral-force illustration.

SubsystemProvisional architectureAcceptance evidence
BalanceTorsion balance, 0.10 m effective lever arm; illustrative inertia 0.002 kg·m² and 100 s period.Measure inertia, lever arm, stiffness, damping, nonlinearity, creep and mechanical resonances. Final suspension design is open.
Force targetPassive reflective coupon; counterweight and trim; no graphene gate in first campaign.Traceable dimensions and masses; measured optical power distribution and absorption.
ReadoutSeparate low-power optical lever and position detector; interferometric upgrade only if measured noise requires it.Calibrate angle versus detector output; characterize beam-pointing drift and probe-beam recoil. A detector resolution is not force uncertainty.
CalibrationIndependent electrostatic actuator and calibrated voltage/capacitance-gradient model; optical force used as the cross-check.F = ½V² dC/dx, including fringe fields, patch/contact potentials and actual geometry. Do not calibrate with the same optical prediction being tested.
VacuumApproximately 400 mm internal chamber diameter to be checked against drawings; dry-backed turbo candidate.Provisional pressure sweep 10⁻¹ to 10⁻³ Pa where attainable; require a measured force plateau, adequate gauges and outgassing control. Reaching a pressure alone is not a pass.
Thermal / mechanicalThermal shield, sample/mount/chamber temperature channels, matched heater and vibration-isolated pump connection.Measure temperature-to-force transfer functions and pump/tilt sensitivity; include thermal lag and reassembly.
Source and containment1064 nm source capable of the 1 W operating point; external attenuation and monitored power.Qualified laser enclosure, interlocks, beam stops and wavelength-specific protection before operation. Freeze spot size and sensor limits.

Calculate the readout scale before choosing hardware

For the illustrative inertia and period, κ = 4π²I/T² = 7.896 × 10⁻⁶ N·m/rad. A 6.671 nN force at 0.10 m gives 84.49 µrad static deflection; a 1 m optical lever gives approximately 169.0 µm reflected-spot displacement. This estimates range, not sensitivity. Suspension thermal noise, measured loss/Q, environmental tilt and readout drift still set the attainable floor.

The settling time is not the pendulum period

For a lightly damped viscous model, the amplitude ring-down time is QT/π. At T = 100 s and an illustrative Q = 100, this is roughly 3,183 s. Structural loss or feedback changes the response. Measure the transfer function before choosing modulation, dwell time or averaging; 280 independent windows cannot be translated into a campaign duration without that evidence.

A budget that must be earned

Target an expanded uncertainty below 10% of the 1 W ideal reference: 0.667 nN. The allocations below combine to u = 0.276 nN and U = 0.552 nN at coverage factor k = 2 if independent. Adding an illustrative thermal/mechanical correlation of 0.6 raises U to 0.602 nN. Actual coverage and covariance must be evaluated from the instrument; unknown effects cannot be assigned zero.

ContributionAllocationEvidence status
Optical prediction0.10 nNProposed standard-uncertainty allocation
Force calibration0.10 nNProposed standard-uncertainty allocation
Statistical mean difference0.12 nNProposed standard-uncertainty allocation
Thermal residual0.15 nNProposed standard-uncertainty allocation
Electrostatic residual0.08 nNProposed standard-uncertainty allocation
Gas residual0.08 nNProposed standard-uncertainty allocation
Mechanical residual0.08 nNProposed standard-uncertainty allocation

Use enough independent data

For a full on/off difference with equal allocation, u = 2σ/√N. If qualified window noise is 1 nN, 280 total independent windows give 0.120 nN statistical standard uncertainty. This is a planning calculation, not a demonstration of independence or a substitute for prospective detection-power analysis. Recalculate when measured drift, autocorrelation and settling are available.

GateProposed pass criterionIf it fails
G0 · design reviewExperimental lead and independent reviewer accept the observable, mechanical model, optical layout, hazards, uncertainty model and interface drawings.Do not purchase integrated hardware.
G1 · reference calibrationIndependent reference recovered over the selected range; pre/post drift stays within the 0.10 nN calibration allocation at the test point.Repair calibration or relax the experiment’s scope.
G2 · nuisance controlsResidual effects and their uncertainties fit the allocated budget; each state-correlated contribution is measured or defensibly bounded.Add controls or stop that configuration.
G3 · optical closureSigned force agrees with measured optical momentum within the combined k=2 interval; expanded uncertainty ≤0.667 nN at the 1 W reference. Check 0.25/0.5/1 W scaling and an appropriate reversal/null configuration.Report discrepancy; do not reinterpret it as new physics.
G4 · repeatabilityThe closure and controls repeat across at least three days and a controlled reassembly using a frozen analysis.Investigate instability before materials integration.
G5 · graphene entryIndependent optical/thermal characterization predicts a resolvable state difference at a demonstrated safe operating point.Keep graphene in optical characterization; no forced transfer to the balance.

Review roles and missing engineering

Christopher Hill owns program priorities. A qualified experimental lead must own mechanical and optical design; a metrologist must review calibration and uncertainty; an independent physicist must challenge the interpretation. These roles remain unfilled. Fabrication drawings, suspension material/dimensions, actuator geometry, control law, measured environmental spectra and installation requirements are still required before procurement.