Input
| Simulation Speedup | |||
| Latitude | |||
| Mass (kg) | Power (W) | ||
|---|---|---|---|
| Airship | |||
| Lifting Gas | |||
| Volume (`m^3`) | |||
| Final Volume (`m^3`) | |||
| Hull Weight (`kg//m^2`) | |||
| Lift/Drag | |||
| Solar | |||
| Power / Weight (W/kg) | |||
| Battery | |||
| Capacity (Wh) | |||
| Energy / Weight (Wh/kg) | |||
| Avionics | |||
| Propulsion | |||
Output
| Time | ||
| Altitude (m) | ||
| Gravity (m/s^2) | `g = ( G M ) / r^2` | |
| Gravitational Force (N) | `g = ( G M ) / r^2` | |
| Pressure (Pa) | ||
| Volume (`m^3`) | `PV = nRT` | |
| Hull Pressure (Pa) | ||
| Buoyancy (N) | `F = Delta rho V` | |
| Velocity (m/s) | ||
| Absolute Velocity (m/s) | ||
| Orbital Velocity (m/s) | `v = sqrt( ( G M ) / r )` | |
| Kinetic Energy (J) | `E = ( m v^2 ) / 2` | |
| Aerodynamic Lift (N) | `F_L = ( rho v^2 A C_L ) / 2` | |
| Aerodynamic Drag (N) | `F_D = ( rho v^2 A C_D ) / 2` | |
| Centrifugal Force (N) | `F = ( m v^2 ) / r` |