Live Clock Stack
UTC Clock--
Local Clock--
Atomic Reference--
CST Ship Clock--
Interstellar Nav Clock--
Mission Elapsed0 s
Mission Inputs
Earth-to-Mars Visual Flight
Earth
Mars
↓
↓
↓
Lower rear exhaust path
Trip Progress
Distance Traveled0 km
Distance Remaining-- km
Current Velocity--
Estimated Real Trip Time--
Simulated Arrival--
Rotational Pulse Chamber Ring
Active Cell--
Phase Angle θₙ--
Pulse Frequency--
Total Pulse Power--
Euler Phase--
θₙ = 2πn / N
Ψₙ(t) = Aₙei(ωt + θₙ)
eiθ = cosθ + i sinθ
Euler phase control organizes the live rotating chamber sequence.
Energy and Mass Readings
Total Craft Mass--
Kinetic Energy Estimate--
Relativistic Energy Estimate--
Mass-Equivalent Energy--
Live Energy Delivered--
Stored Energy Rate--
E = mc²
m = E / c²
Eₖ = ½Mv²
Eᵣₑₗ = (γ − 1)Mc²
γ = 1 / √(1 − v²/c²)
Propulsion and Dual Engine Output
Throttle α--
Effective Power--
Power Per Engine--
Estimated Thrust--
Mass Flow Model--
Engine BalanceLeft = Right
P ≈ N Eₚ f
Pₑff = α N Eₚ f
F = ṁvₑ
τ = r(Fᴸ − Fᴿ)
Lower Aft Reaction and Radiation Exhaust
Reaction ZoneLower / Aft
Radiation StorageNone
Rear Exhaust Flow--
Converted Energy Flow--
Crew Flux Estimate--
Shield Attenuation--
dEₛₜₒᵣₑd / dt ≈ 0
Egenerated → Erear exhaust + Econverted + Eloss
Φcrew = Φ₀e−μx / r²