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Formula Card

Every formula the handbook derives, on one page — each with the reference build's value so you can sanity-check your own arithmetic against a known-good answer. Derivations live in the linked modules; this card is for the field and the spreadsheet. (5″ reference: 650 g, 6S, 1855 KV, Gemfan 51466 — the build page assembles it.)

Lift & power — Module 2

FormulaAnswersReference build
TWR=Tmaxmg\text{TWR} = \dfrac{T_\text{max}}{m\,g}Can it accelerate? (freestyle: 8–12)6000/650=9.26000/650 = 9.2
throttlehover1/TWR\text{throttle}_\text{hover} \approx \sqrt{1/\text{TWR}}Where hover sits on the stick1/9.233 %\sqrt{1/9.2} \approx 33\ \%
Pideal=T3/22ρAP_\text{ideal} = \dfrac{T^{3/2}}{\sqrt{2\rho A}}Momentum-theory floor for hover power46\approx 46 W ideal → ≈ 122 W real at the battery
T=CTρn2D4T = C_T\,\rho\,n^2 D^4, P=CPρn3D5P = C_P\,\rho\,n^3 D^5Why big slow props win on efficiencythrust ∝ RPM², power ∝ RPM³

Motors — Module 5

FormulaAnswersReference build
RPMno-load=KV×V\text{RPM}_\text{no-load} = KV \times VTop of the rev range1855×25.2467001855 \times 25.2 \approx 46\,700
Kt=9.549/KVK_t = 9.549 / KV (mN·m/A)Torque per amp — predicts current5.15\approx 5.15 mN·m/A
vpitch=RPM×pitchv_\text{pitch} = \text{RPM} \times \text{pitch}Hard upper bound on speed32700×4.6623232\,700 \times 4.66''\approx 232 km/h (real: 130–150)

Energy & endurance — Module 6

FormulaAnswersReference build
E=Vnom×AhE = V_\text{nom} \times \text{Ah}What actually flies (energy, not capacity)22.2×1.3=28.922.2 \times 1.3 = 28.9 Wh
t=0.8E/Pavgt = 0.8\,E / P_\text{avg}Honest flight time (80 % usable)11.4 min hover; 3–5 min freestyle
ΔV=IRint\Delta V = I\,R_\text{int}Punch-out sag on the OSD120×0.021=2.5120 \times 0.021 = 2.5 V
Pheat=I2RintP_\text{heat} = I^2 R_\text{int}Why packs land warm302\approx 302 W inside the pack
mb=2m0m_b = 2\,m_0Endurance-optimal battery massderivation in Module 6; plateau is wide
FormulaAnswersReference numbers
FSPL=32.44+20log10fMHz+20log10dkm\text{FSPL} = 32.44 + 20\log_{10} f_\text{MHz} + 20\log_{10} d_\text{km}Free-space path loss2.4 GHz @ 2 km ≈ 106 dB
margin =Ptx+GantFSPLSrx= P_\text{tx} + G_\text{ant} - \text{FSPL} - S_\text{rx}Will the link hold?≈ 26 dB at 250 Hz (Receiver)
every −3 dB sensitivity≈ 1.4× range250 Hz → 50 Hz ≈ 2× range

Tuning & filters — Module 9

FormulaAnswersReference build
fmotor=RPM/60f_\text{motor} = \text{RPM}/60Where the spectrogram ridge sits300 Hz at hover → 533 Hz full throttle
blade-pass =fmotor×= f_\text{motor} \times bladesThe second ridge900–1600 Hz (3-blade)
td=12πfct_d = \dfrac{1}{2\pi f_c}Delay cost of a PT1 lowpass100 Hz → 1.59 ms
Δffnotch/Q\Delta f \approx f_\text{notch}/QHow surgical a notch is300 Hz, Q=10 → ±15 Hz

Build & integration — Module 10

FormulaAnswersReference build
xCG=imixiimix_{CG} = \dfrac{\sum_i m_i x_i}{\sum_i m_i}Where the pack goesbattery over CG, always
fn=12πk/mf_n = \dfrac{1}{2\pi}\sqrt{k/m}Soft-mount resonancetarget 60–100 Hz
Rsystem=iRiR_\text{system} = \prod_i R_iWhy one joint ruins a build0.99940=0.9610.999^{40} = 0.961 — 1 failure per 26 flights
How to use this card

Every row is a one-minute sanity check: put your numbers in, and if the answer lands far from the reference column's ballpark, one of your inputs is wrong — usually a unit. The modules linked in each section show the full worked examples.