Explore our open-source aerospace tools, calculators, and simulators
Calculate Mach number and local speed of sound based on airspeed and altitude.
Determine the Reynolds number for various fluid flow scenarios and conditions.
Calculate property changes across a normal shock wave in supersonic flow conditions.
Calculate pressure, temperature, and density ratios across an isentropic flow.
Calculate lift and drag forces, coefficients, stall speed estimation, and basic aerodynamic performance.
Calculate properties across oblique shock waves based on upstream conditions.
Determine flow turning and property changes through an expansion fan.
Estimate CD0, induced drag factor, and target drag from two parabolic drag-polar points.
Estimate flat-plate laminar/turbulent skin-friction coefficient and drag.
Calculate compressible-flow stagnation temperature and total-to-static ratios from Mach number.
Generate NACA 4/5-digit coordinates and basic aerodynamic metrics.
Calculate drag coefficient, pressure distribution, and flow characteristics around a sphere for various Reynolds numbers.
Estimate 3D wing lift-curve slope from 2D airfoil slope, aspect ratio, and span efficiency.
Estimate laminar and turbulent flat-plate boundary-layer thickness and skin-friction coefficients.
Apply the subsonic Prandtl-Glauert compressibility correction to lift or pressure coefficients.
Calculate atmospheric properties (altitude, pressure, temp, density) using the ISA model.
Calculate aircraft weight breakdown, fuel fractions, payload capacity, weight fraction relationships, and wing loading (W/S).
Calculate maximum lift-to-drag ratio, optimal velocities for range and endurance, and basic aerodynamic performance characteristics.
Calculate q-bar and sea-level equivalent airspeed from velocity and air density.
Analyze climb rates, angles, time to climb, service ceiling, descent planning, and glide performance characteristics.
Generate V-n diagrams, flight envelopes, gust load factors, maneuver limits, and performance boundary analysis.
Calculate aircraft range and endurance using Breguet equations, optimal cruise conditions, and fuel flow analysis.
Compute balanced field length and runway distance requirements.
Calculate incompressible airspeed from pitot-static differential pressure and density.
Turn radius, bank angle, and load factor for specified speed and rate.
Digital E6B: wind correction, TAS, density altitude, and more.
Size wing loading and stall speed from aircraft mass, wing area, density, and maximum lift coefficient.
Estimate still-air glide range, glide time, and sink rate from altitude, speed, and lift-to-drag ratio.
Estimate service ceiling from sea-level climb rate and climb-rate lapse with altitude.
Calculate aircraft or rocket static margin from center of gravity, neutral point, and reference chord/diameter.
Estimate maximum radar detection range based on system parameters.
Compute one-way RF received power, carrier-to-noise ratio, data capacity, and link margin.
Calculate antenna gain, beamwidth, and directivity for parabolic and horn antennas.
Calculate signal attenuation in free space for various frequencies and distances.
Calculate frequency shifts due to relative motion between transmitter and receiver.
Calculate system noise figure and noise temperature for cascaded amplifiers.
Calculate modulation index and bandwidth for AM, FM, and PM signals.
Calculate BER for various modulation schemes and signal-to-noise ratios.
Calculate signal loss due to polarization mismatch between antennas.
Combine gaseous, rain, cloud/fog, and miscellaneous atmospheric losses over a slant path.
Calculate beam steering, normalized pattern, and beamwidth for uniform linear antenna arrays.
Calculate theoretical channel capacity using Shannon's theorem.
Convert between common units frequently used in aerospace engineering calculations.
Convert between AU, km, m, light-years, parsecs, and lunar distance.
Convert between WGS84 geodetic, ECEF, UTM, and MGRS coordinates.
Advanced scientific calculator powered by Desmos.
Calculate costs vs quantities, tool costs vs production amounts, and economic analysis for aerospace projects.
Roll up subsystem masses, contingencies, propellant, system margin, and launch capacity margin.
Size spacecraft solar-array and battery capacity from orbital sunlight, eclipse, load, and margins.
Calculate circular-orbit eclipse duration from altitude, beta angle, and central-body parameters.
Calculate radiative equilibrium temperature from absorbed power, area, and emissivity.
Calculate damping ratio response metrics such as overshoot, settling time, and damped natural frequency.
Estimate reaction-wheel angular momentum storage, wheel inertia, and kinetic energy for an attitude slew torque.
Calculate circular-orbit period, velocity, escape speed, and mean motion around common or custom bodies.
Calculate orbital velocity and specific energy from radius, semi-major axis, and gravitational parameter.
Calculate the required delta-v for efficient Hohmann transfer orbital maneuvers.
Evaluate three-impulse bi-elliptic transfer delta-v, time of flight, and Hohmann comparison.
Calculate Laplace sphere-of-influence radius for patched-conic mission design.
Calculate Hill radius and rough stable satellite orbit limits from orbit and mass ratio.
Input delta-v values for mission phases to calculate total requirements.
Design the J2-driven inclination needed for a sun-synchronous low Earth orbit.
Compute nodal precession due to J2 for sun-synchronous and other LEO orbits.
Minimize delta-v for inclination/RAAN changes and combined maneuvers.
Estimate stagnation-point reentry convective heating with the Sutton-Graves correlation.
Convert inertial position and velocity vectors into classical orbital elements and classify orbit geometry.
Solve Kepler's equation for elliptical orbits and convert between mean, eccentric, and true anomaly.
Analyze hyperbolic orbits, escape trajectories, and flyby missions with hyperbolic excess velocity.
Estimate inertial launch azimuth needed to reach a target inclination from a launch latitude.
Estimate a one-revolution phasing orbit and two-burn delta-v for circular-orbit rendezvous timing.
Estimate orbit count and longitude shift for a repeating ground-track cycle.
Estimate circular-orbit semi-major-axis decay rate from drag area, mass, density, and velocity.
Convert characteristic energy into hyperbolic excess speed and parking-orbit departure delta-v.
Calculate pixel resolution, coverage area, and footprint for aerial/satellite photography missions.
Calculate aircraft angular tracking rate and exposure limit from speed, range, and crossing angle.
Calculate satellite streak length in arcseconds and pixels for camera exposures.
Calculate effective focal length, focal ratio, magnification, and exit pupil.
Calculate diffraction-limited angular resolution and ground spot size for circular apertures.
Estimate rocket delta-v performance using the Tsiolkovsky rocket equation.
Calculate propellant mass fraction based on initial and final masses.
Calculate thrust-to-weight ratio for aircraft or rockets.
Convert specific impulse values between seconds and velocity units.
Calculate propeller advance ratio, thrust coefficient, power coefficient, and efficiency.
Calculate ideal converging-diverging nozzle area ratio, mass flow, thrust, and Isp.
Analyze ideal Brayton cycle temperatures, work, thermal efficiency, and back-work ratio.
Estimate electric-thruster thrust, mass flow, total impulse, and propellant from power and Isp.
Calculate TSFC from fuel mass flow and thrust in SI and customary units.
Estimate induced velocity, ideal hover power, and disk loading from momentum theory.
Calculate propellant mass flow, burn time, and total impulse from thrust, Isp, and propellant mass.
Estimate hydraulic and shaft power for a pump from mass flow, pressure rise, density, and efficiency.
Convert rocket specific impulse into effective exhaust velocity, mass flow, and thrust power.
Calculate rotor tip speed, corrected speed, and tip Mach number for compressor preliminary checks.
Deflection, slope, shear, and moment for common beam load cases.
Euler buckling and effective length factors for structural members.
Allowables and margins for rivets/bolts in single- and double-shear.
Hoop and longitudinal stresses for thin/thick-walled cylinders and spheres.
Kt values for common geometric features like holes, fillets, and notches.
Estimate high-cycle fatigue life from Basquin stress-life constants.
Shear stress and angle of twist for circular and non-circular cross-sections.
Calculate safety factors and margins of safety for structural designs.
First mode natural frequency for beams, plates, and simple structures.
Estimate constrained thermal stress and force from modulus, expansion coefficient, temperature change, and area.
Calculate plane-stress von Mises equivalent stress and safety factor.
Estimate elastic local buckling stress for a thin rectangular plate.
Calculate thin-wall shear flow and shear stress from shear force, first moment, inertia, and wall thickness.
Estimate direct and torsional shear per fastener for a circular rivet or bolt group.
Compare aerospace materials by specific stiffness, specific strength, material indices, and cost-adjusted performance.
Estimate endurance from battery capacity, payload, and environment.
Plan UAV mapping line spacing, image interval, photo count, and flight time from camera overlap.
Estimate pack voltage, capacity, and C-rating for mission profiles.
Explore our open-source aerospace tools, calculators, and simulators
Calculate Mach number and local speed of sound based on airspeed and altitude.
Determine the Reynolds number for various fluid flow scenarios and conditions.
Calculate property changes across a normal shock wave in supersonic flow conditions.
Calculate pressure, temperature, and density ratios across an isentropic flow.
Calculate lift and drag forces, coefficients, stall speed estimation, and basic aerodynamic performance.
Calculate properties across oblique shock waves based on upstream conditions.
Determine flow turning and property changes through an expansion fan.
Estimate CD0, induced drag factor, and target drag from two parabolic drag-polar points.
Estimate flat-plate laminar/turbulent skin-friction coefficient and drag.
Calculate compressible-flow stagnation temperature and total-to-static ratios from Mach number.
Generate NACA 4/5-digit coordinates and basic aerodynamic metrics.
Calculate drag coefficient, pressure distribution, and flow characteristics around a sphere for various Reynolds numbers.
Estimate 3D wing lift-curve slope from 2D airfoil slope, aspect ratio, and span efficiency.
Estimate laminar and turbulent flat-plate boundary-layer thickness and skin-friction coefficients.
Apply the subsonic Prandtl-Glauert compressibility correction to lift or pressure coefficients.
Calculate atmospheric properties (altitude, pressure, temp, density) using the ISA model.
Calculate aircraft weight breakdown, fuel fractions, payload capacity, weight fraction relationships, and wing loading (W/S).
Calculate maximum lift-to-drag ratio, optimal velocities for range and endurance, and basic aerodynamic performance characteristics.
Calculate q-bar and sea-level equivalent airspeed from velocity and air density.
Analyze climb rates, angles, time to climb, service ceiling, descent planning, and glide performance characteristics.
Generate V-n diagrams, flight envelopes, gust load factors, maneuver limits, and performance boundary analysis.
Calculate aircraft range and endurance using Breguet equations, optimal cruise conditions, and fuel flow analysis.
Compute balanced field length and runway distance requirements.
Calculate incompressible airspeed from pitot-static differential pressure and density.
Turn radius, bank angle, and load factor for specified speed and rate.
Digital E6B: wind correction, TAS, density altitude, and more.
Size wing loading and stall speed from aircraft mass, wing area, density, and maximum lift coefficient.
Estimate still-air glide range, glide time, and sink rate from altitude, speed, and lift-to-drag ratio.
Estimate service ceiling from sea-level climb rate and climb-rate lapse with altitude.
Calculate aircraft or rocket static margin from center of gravity, neutral point, and reference chord/diameter.
Estimate maximum radar detection range based on system parameters.
Compute one-way RF received power, carrier-to-noise ratio, data capacity, and link margin.
Calculate antenna gain, beamwidth, and directivity for parabolic and horn antennas.
Calculate signal attenuation in free space for various frequencies and distances.
Calculate frequency shifts due to relative motion between transmitter and receiver.
Calculate system noise figure and noise temperature for cascaded amplifiers.
Calculate modulation index and bandwidth for AM, FM, and PM signals.
Calculate BER for various modulation schemes and signal-to-noise ratios.
Calculate signal loss due to polarization mismatch between antennas.
Combine gaseous, rain, cloud/fog, and miscellaneous atmospheric losses over a slant path.
Calculate beam steering, normalized pattern, and beamwidth for uniform linear antenna arrays.
Calculate theoretical channel capacity using Shannon's theorem.
Convert between common units frequently used in aerospace engineering calculations.
Convert between AU, km, m, light-years, parsecs, and lunar distance.
Convert between WGS84 geodetic, ECEF, UTM, and MGRS coordinates.
Advanced scientific calculator powered by Desmos.
Calculate costs vs quantities, tool costs vs production amounts, and economic analysis for aerospace projects.
Roll up subsystem masses, contingencies, propellant, system margin, and launch capacity margin.
Size spacecraft solar-array and battery capacity from orbital sunlight, eclipse, load, and margins.
Calculate circular-orbit eclipse duration from altitude, beta angle, and central-body parameters.
Calculate radiative equilibrium temperature from absorbed power, area, and emissivity.
Calculate damping ratio response metrics such as overshoot, settling time, and damped natural frequency.
Estimate reaction-wheel angular momentum storage, wheel inertia, and kinetic energy for an attitude slew torque.
Calculate circular-orbit period, velocity, escape speed, and mean motion around common or custom bodies.
Calculate orbital velocity and specific energy from radius, semi-major axis, and gravitational parameter.
Calculate the required delta-v for efficient Hohmann transfer orbital maneuvers.
Evaluate three-impulse bi-elliptic transfer delta-v, time of flight, and Hohmann comparison.
Calculate Laplace sphere-of-influence radius for patched-conic mission design.
Calculate Hill radius and rough stable satellite orbit limits from orbit and mass ratio.
Input delta-v values for mission phases to calculate total requirements.
Design the J2-driven inclination needed for a sun-synchronous low Earth orbit.
Compute nodal precession due to J2 for sun-synchronous and other LEO orbits.
Minimize delta-v for inclination/RAAN changes and combined maneuvers.
Estimate stagnation-point reentry convective heating with the Sutton-Graves correlation.
Convert inertial position and velocity vectors into classical orbital elements and classify orbit geometry.
Solve Kepler's equation for elliptical orbits and convert between mean, eccentric, and true anomaly.
Analyze hyperbolic orbits, escape trajectories, and flyby missions with hyperbolic excess velocity.
Estimate inertial launch azimuth needed to reach a target inclination from a launch latitude.
Estimate a one-revolution phasing orbit and two-burn delta-v for circular-orbit rendezvous timing.
Estimate orbit count and longitude shift for a repeating ground-track cycle.
Estimate circular-orbit semi-major-axis decay rate from drag area, mass, density, and velocity.
Convert characteristic energy into hyperbolic excess speed and parking-orbit departure delta-v.
Calculate pixel resolution, coverage area, and footprint for aerial/satellite photography missions.
Calculate aircraft angular tracking rate and exposure limit from speed, range, and crossing angle.
Calculate satellite streak length in arcseconds and pixels for camera exposures.
Calculate effective focal length, focal ratio, magnification, and exit pupil.
Calculate diffraction-limited angular resolution and ground spot size for circular apertures.
Estimate rocket delta-v performance using the Tsiolkovsky rocket equation.
Calculate propellant mass fraction based on initial and final masses.
Calculate thrust-to-weight ratio for aircraft or rockets.
Convert specific impulse values between seconds and velocity units.
Calculate propeller advance ratio, thrust coefficient, power coefficient, and efficiency.
Calculate ideal converging-diverging nozzle area ratio, mass flow, thrust, and Isp.
Analyze ideal Brayton cycle temperatures, work, thermal efficiency, and back-work ratio.
Estimate electric-thruster thrust, mass flow, total impulse, and propellant from power and Isp.
Calculate TSFC from fuel mass flow and thrust in SI and customary units.
Estimate induced velocity, ideal hover power, and disk loading from momentum theory.
Calculate propellant mass flow, burn time, and total impulse from thrust, Isp, and propellant mass.
Estimate hydraulic and shaft power for a pump from mass flow, pressure rise, density, and efficiency.
Convert rocket specific impulse into effective exhaust velocity, mass flow, and thrust power.
Calculate rotor tip speed, corrected speed, and tip Mach number for compressor preliminary checks.
Deflection, slope, shear, and moment for common beam load cases.
Euler buckling and effective length factors for structural members.
Allowables and margins for rivets/bolts in single- and double-shear.
Hoop and longitudinal stresses for thin/thick-walled cylinders and spheres.
Kt values for common geometric features like holes, fillets, and notches.
Estimate high-cycle fatigue life from Basquin stress-life constants.
Shear stress and angle of twist for circular and non-circular cross-sections.
Calculate safety factors and margins of safety for structural designs.
First mode natural frequency for beams, plates, and simple structures.
Estimate constrained thermal stress and force from modulus, expansion coefficient, temperature change, and area.
Calculate plane-stress von Mises equivalent stress and safety factor.
Estimate elastic local buckling stress for a thin rectangular plate.
Calculate thin-wall shear flow and shear stress from shear force, first moment, inertia, and wall thickness.
Estimate direct and torsional shear per fastener for a circular rivet or bolt group.
Compare aerospace materials by specific stiffness, specific strength, material indices, and cost-adjusted performance.
Estimate endurance from battery capacity, payload, and environment.
Plan UAV mapping line spacing, image interval, photo count, and flight time from camera overlap.
Estimate pack voltage, capacity, and C-rating for mission profiles.