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Aerospace Tools

Explore our open-source aerospace tools, calculators, and simulators

Aerodynamics

Mach Number

Calculate Mach number and local speed of sound based on airspeed and altitude.

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Reynolds Number

Determine the Reynolds number for various fluid flow scenarios and conditions.

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Normal Shock

Calculate property changes across a normal shock wave in supersonic flow conditions.

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Isentropic Flow

Calculate pressure, temperature, and density ratios across an isentropic flow.

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Lift & Drag

Calculate lift and drag forces, coefficients, stall speed estimation, and basic aerodynamic performance.

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Oblique Shock

Calculate properties across oblique shock waves based on upstream conditions.

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Prandtl-Meyer Expansion

Determine flow turning and property changes through an expansion fan.

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Drag Polar Estimator

Estimate CD0, induced drag factor, and target drag from two parabolic drag-polar points.

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Skin Friction Estimator

Estimate flat-plate laminar/turbulent skin-friction coefficient and drag.

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Stagnation Temperature

Calculate compressible-flow stagnation temperature and total-to-static ratios from Mach number.

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Airfoil Generator (NACA)

Generate NACA 4/5-digit coordinates and basic aerodynamic metrics.

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Sphere Flow

Calculate drag coefficient, pressure distribution, and flow characteristics around a sphere for various Reynolds numbers.

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Finite Wing Lift Slope

Estimate 3D wing lift-curve slope from 2D airfoil slope, aspect ratio, and span efficiency.

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Boundary Layer Thickness

Estimate laminar and turbulent flat-plate boundary-layer thickness and skin-friction coefficients.

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Prandtl-Glauert Correction

Apply the subsonic Prandtl-Glauert compressibility correction to lift or pressure coefficients.

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Astronomy
Atmospheric & Flight

ISA Atmosphere

Calculate atmospheric properties (altitude, pressure, temp, density) using the ISA model.

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Aircraft Weight Sizing

Calculate aircraft weight breakdown, fuel fractions, payload capacity, weight fraction relationships, and wing loading (W/S).

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Aircraft Performance Basics

Calculate maximum lift-to-drag ratio, optimal velocities for range and endurance, and basic aerodynamic performance characteristics.

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Dynamic Pressure

Calculate q-bar and sea-level equivalent airspeed from velocity and air density.

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Climb & Descent Performance

Analyze climb rates, angles, time to climb, service ceiling, descent planning, and glide performance characteristics.

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Performance Envelopes

Generate V-n diagrams, flight envelopes, gust load factors, maneuver limits, and performance boundary analysis.

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Range & Endurance Analysis

Calculate aircraft range and endurance using Breguet equations, optimal cruise conditions, and fuel flow analysis.

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Takeoff & Landing Distance

Compute balanced field length and runway distance requirements.

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Pitot-Static Airspeed

Calculate incompressible airspeed from pitot-static differential pressure and density.

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Coordinated Turn

Turn radius, bank angle, and load factor for specified speed and rate.

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E6B Flight Computer

Digital E6B: wind correction, TAS, density altitude, and more.

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Wing Loading & Stall Speed

Size wing loading and stall speed from aircraft mass, wing area, density, and maximum lift coefficient.

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Aircraft Glide Range

Estimate still-air glide range, glide time, and sink rate from altitude, speed, and lift-to-drag ratio.

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Service Ceiling Estimator

Estimate service ceiling from sea-level climb rate and climb-rate lapse with altitude.

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Static Margin

Calculate aircraft or rocket static margin from center of gravity, neutral point, and reference chord/diameter.

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Communications
General Utilities
Mission Planning
Navigation
Orbital Mechanics

Circular Orbit

Calculate circular-orbit period, velocity, escape speed, and mean motion around common or custom bodies.

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Vis-Viva Equation

Calculate orbital velocity and specific energy from radius, semi-major axis, and gravitational parameter.

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Hohmann Transfer

Calculate the required delta-v for efficient Hohmann transfer orbital maneuvers.

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Bi-Elliptic Transfer

Evaluate three-impulse bi-elliptic transfer delta-v, time of flight, and Hohmann comparison.

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Sphere of Influence

Calculate Laplace sphere-of-influence radius for patched-conic mission design.

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Hill Sphere

Calculate Hill radius and rough stable satellite orbit limits from orbit and mass ratio.

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Delta-V Budget

Input delta-v values for mission phases to calculate total requirements.

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Sun-Synchronous Orbit Designer

Design the J2-driven inclination needed for a sun-synchronous low Earth orbit.

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RAAN Drift

Compute nodal precession due to J2 for sun-synchronous and other LEO orbits.

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Plane Change Optimizer

Minimize delta-v for inclination/RAAN changes and combined maneuvers.

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Reentry Heating & Corridor

Estimate stagnation-point reentry convective heating with the Sutton-Graves correlation.

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Orbital Elements

Convert inertial position and velocity vectors into classical orbital elements and classify orbit geometry.

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Kepler's Equation Solver

Solve Kepler's equation for elliptical orbits and convert between mean, eccentric, and true anomaly.

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Hyperbolic Trajectory

Analyze hyperbolic orbits, escape trajectories, and flyby missions with hyperbolic excess velocity.

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Launch Azimuth

Estimate inertial launch azimuth needed to reach a target inclination from a launch latitude.

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Phasing Maneuver

Estimate a one-revolution phasing orbit and two-burn delta-v for circular-orbit rendezvous timing.

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Ground Track Repeat Cycle

Estimate orbit count and longitude shift for a repeating ground-track cycle.

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Orbital Drag Decay Estimator

Estimate circular-orbit semi-major-axis decay rate from drag area, mass, density, and velocity.

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C3 Energy

Convert characteristic energy into hyperbolic excess speed and parking-orbit departure delta-v.

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Photography / Imaging
Propulsion

Rocket Equation

Estimate rocket delta-v performance using the Tsiolkovsky rocket equation.

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Propellant Mass Fraction

Calculate propellant mass fraction based on initial and final masses.

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Thrust-to-Weight Ratio

Calculate thrust-to-weight ratio for aircraft or rockets.

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Specific Impulse Converter

Convert specific impulse values between seconds and velocity units.

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Propeller Performance Estimator

Calculate propeller advance ratio, thrust coefficient, power coefficient, and efficiency.

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Nozzle Design (C-D)

Calculate ideal converging-diverging nozzle area ratio, mass flow, thrust, and Isp.

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Brayton Cycle Analyzer

Analyze ideal Brayton cycle temperatures, work, thermal efficiency, and back-work ratio.

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Electric Propulsion Sizing

Estimate electric-thruster thrust, mass flow, total impulse, and propellant from power and Isp.

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Thrust-Specific Fuel Consumption

Calculate TSFC from fuel mass flow and thrust in SI and customary units.

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Actuator Disk Hover

Estimate induced velocity, ideal hover power, and disk loading from momentum theory.

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Rocket Burn Time

Calculate propellant mass flow, burn time, and total impulse from thrust, Isp, and propellant mass.

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Turbopump Power Estimator

Estimate hydraulic and shaft power for a pump from mass flow, pressure rise, density, and efficiency.

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Effective Exhaust Velocity

Convert rocket specific impulse into effective exhaust velocity, mass flow, and thrust power.

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Compressor Tip Speed

Calculate rotor tip speed, corrected speed, and tip Mach number for compressor preliminary checks.

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Structures

Beam Bending & Deflection

Deflection, slope, shear, and moment for common beam load cases.

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Column Buckling

Euler buckling and effective length factors for structural members.

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Fastener Shear/Bearing

Allowables and margins for rivets/bolts in single- and double-shear.

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Pressure Vessel Stress

Hoop and longitudinal stresses for thin/thick-walled cylinders and spheres.

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Stress Concentration Factor

Kt values for common geometric features like holes, fillets, and notches.

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Fatigue Life Estimator

Estimate high-cycle fatigue life from Basquin stress-life constants.

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Torsion

Shear stress and angle of twist for circular and non-circular cross-sections.

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Safety Factor & Margin

Calculate safety factors and margins of safety for structural designs.

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Natural Frequency

First mode natural frequency for beams, plates, and simple structures.

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Thermal Stress

Estimate constrained thermal stress and force from modulus, expansion coefficient, temperature change, and area.

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Von Mises Stress

Calculate plane-stress von Mises equivalent stress and safety factor.

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Plate Buckling

Estimate elastic local buckling stress for a thin rectangular plate.

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Shear Flow

Calculate thin-wall shear flow and shear stress from shear force, first moment, inertia, and wall thickness.

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Rivet Group Load Distribution

Estimate direct and torsional shear per fastener for a circular rivet or bolt group.

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Material Index Explorer

Compare aerospace materials by specific stiffness, specific strength, material indices, and cost-adjusted performance.

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UAV Operations