UFO Travel Calculator

Model interplanetary or interstellar travel time, relativistic elapsed time, and efficiency-adjusted energy requirements.

Calculate a spacecraft journey
Define positions, cruise speed, system efficiency, continuous power, and each acceleration phase.

About the UFO travel model

The UFO Travel Calculator is an educational spacecraft journey model inspired by interplanetary and interstellar travel. It starts with the absolute difference between starting and target positions, then divides that distance by a constant cruise speed. Because a real craft cannot jump instantly to cruise velocity, the entered acceleration time is included once for departure and once for deceleration at the destination. The total coordinate time is therefore cruise time plus two acceleration phases. This intentionally simple model makes assumptions visible rather than claiming to simulate an unknown propulsion technology. Relativity matters when speed becomes a substantial fraction of the speed of light. The calculator restricts velocity to less than 299,792.458 kilometres per second and computes the Lorentz factor γ = 1/√(1 − v²/c²). Coordinate time is the duration measured in the starting frame. Dividing it by γ estimates elapsed time aboard a constantly moving craft. At ordinary spacecraft speeds the factor is almost one, so the two times are effectively equal. Near light speed the traveler's elapsed time becomes shorter, although observers in the starting frame still measure the full coordinate duration. The energy output uses entered continuous power rather than attempting to infer kinetic energy from an unspecified spacecraft mass. Megawatts multiplied by operating hours gives megawatt-hours. Dividing by fractional system efficiency estimates the input energy needed to deliver that operating power. This quantity is not propellant mass. Converting energy to fuel would require a specific energy density, conversion process, reserve policy, tank mass, and often the relativistic rocket equation. Acceleration power may also differ radically from cruise power, so the estimate should be treated as a transparent scenario metric. Real mission design is much more complex. Trajectories curve under gravity, planetary positions change, acceleration may be continuous, and propulsion systems have limits on thrust, waste heat, exhaust velocity, and available energy. Relativistic acceleration requires integrating velocity over time rather than simply adding fixed-duration phases. The calculator nevertheless helps users compare scales, see why distant destinations remain challenging, and explore how speed and efficiency affect a hypothetical journey. It is not evidence that faster-than-light or unidentified craft exist, and it cannot establish engineering feasibility. Use verified ephemerides, propulsion data, numerical trajectory software, and professional mission analysis for real aerospace work.

Space travel examples

The examples use constant cruise speed and equal acceleration and deceleration periods.

JourneyCoordinate timeAssumption
40 million km at 50,000 km/s0.222 cruise hoursSimplified Mars separation
4.13 × 10¹³ km at 150,000 km/s8.73 yearsApproximate Alpha Centauri range
5 billion km at 75,000 km/s18.52 hoursOuter solar-system scale

How to model a journey

  1. Enter starting and target positions in kilometres.
  2. Choose a positive cruise speed below the speed of light.
  3. Enter propulsion efficiency, continuous power, and one acceleration-phase duration.
  4. Select Calculate and compare coordinate time, traveler time, and input energy.

Frequently asked questions

Does this calculator support faster-than-light speed?

No. Special relativity does not permit a massive craft to reach or exceed light speed, so the input is restricted below c.

What is traveler elapsed time?

It is coordinate time divided by the Lorentz factor in this constant-speed model. It represents idealized proper time aboard the moving craft.

Is energy required the same as fuel mass?

No. The result is efficiency-adjusted electrical or system energy in megawatt-hours, while fuel mass requires a specified energy density and propulsion model.

Why is acceleration time counted twice?

The model reserves one equal period to accelerate and another to decelerate. This is a simple allowance and does not integrate a changing velocity profile.

Can this plan a real space mission?

No. Real missions require orbital mechanics, changing celestial positions, propulsion constraints, thermal analysis, and validated trajectory software.