Aviation & Aerospace
AviationCalcs
Engineering calculators for PPL pilots and aerospace engineering students.
PPL & Pilot
Calculators for the private pilot license and aerial navigation.
Aerospace Engineering
Aerodynamics, performance, propulsion and orbital mechanics.
Flight Briefing Generator
All-in-one pre-flight briefing. Enter origin, destination and aircraft data to get live weather, route, fuel and performance in a single document.
METAR / TAF Decoder
SIGMET Decoder
Cloud Base Estimator
Density Altitude
Cloud Base + Density Altitude
ISA Atmosphere
Headings — True / Magnetic / Compass
Wind Correction Angle (WCA) & Ground Speed
Great Circle Distance
Holding Pattern
IAS ↔ TAS
Takeoff & Landing Distance
Cessna 172S — POH §5 (BEFA / Cessna, Rev. 2019)
Cessna 152 — POH §5 (Wayman Aviation / Cessna)
PA-28-161 Warrior II — POH §5 (Basic6Aviation / Piper, VB-1180, 1982)
PA-28-181 Archer III — POH §5 (FoxFlying / Piper, VB-1563, 1994/1998) — values interpolated from charts
Diamond DA40 — Tables extracted from official POH §5 (diamondaviators.net)
Robin DR400/180R — POH Supplement §5 Tablas 5-2/5-13 (Robin / EASA, Issue 3, Jul 2014)
SOCATA TB10 Tobago — POH §4 via euroga.org ⚠️ no direct PDF available — verify against aircraft POH
Tecnam P2002 Sierra MkII — Flight Manual §4 (Delta Aviation / Tecnam, Rev.4, 2008) · Base conditions: dry/firm grass (POH standard); paved runway ≈ 6% less ground roll
Fuel Requirements
Mach Number
Mach reference — critical speeds
| Aircraft | Type | Cruise | MMO / Max |
|---|---|---|---|
| Airbus A320 | Narrowbody jet | M0.78 | M0.82 |
| Boeing 737 | Narrowbody jet | M0.79 | M0.82 |
| Airbus A330 | Widebody jet | M0.82 | M0.86 |
| Boeing 787 | Widebody jet | M0.85 | M0.90 |
| Airbus A350 | Widebody jet | M0.85 | M0.89 |
| Boeing 747 | Widebody jet | M0.85 | M0.92 |
| Boeing 777 | Widebody jet | M0.84 | M0.89 |
| Concorde | Supersonic airliner | M2.02 | M2.02 |
| F-16 Fighting Falcon | Fighter jet | — | M2.05 |
| F-22 Raptor | Fighter jet | — | M2.25 |
| SR-71 Blackbird | Recon aircraft | M3.2 | M3.3 |
| X-15 | Experimental | — | M6.7 |
| Source: Wikipedia | |||
Reynolds Number
Lift & Drag
Stall Speed
ISA Atmosphere
Hohmann Transfer
Vis-Viva — Orbital Parameters
Multi-Stage Rocket Staging
ms (structural mass) = dry mass of that stage only — tanks, engines, interstage structure. It does not include propellant or upper stages.
Model assumptions: ideal vacuum, instantaneous burns, constant Isp per stage. Real launches add ~1.5–2 km/s of gravity & drag losses not accounted for here.
Tsiolkovsky Rocket Equation
Specific Impulse (Isp)
Breguet Range Equation
Load Factor
Alternate Airports
Flight Briefing Generator
⚠️ For training and reference only. Always verify data against official sources (AIP, NOTAMs, aircraft POH/AFM) before flight.
About AviationCalcs
AviationCalcs is a free, browser-based suite of precision calculators for PPL students and Aerospace engineering students. No sign-up, no ads, no tracking — just the tools.
PPL & Pilot
Tools for the Private Pilot Licence and aerial navigation
- METAR / TAF Decoder
- SIGMET Decoder
- Cloud Base & Density Altitude
- ISA Standard Atmosphere
- Headings (True / Magnetic / Compass)
- Wind Correction Angle & Ground Speed
- Great Circle Distance
- Holding Pattern
- Alternate Airports
- IAS ↔ TAS Converter
- Takeoff & Landing (TOLD)
- Fuel Requirements
- Flight Briefing Generator
Aerospace
Engineering calculators for aerodynamics, propulsion & orbital mechanics
- Mach Number
- Reynolds Number
- Lift & Drag
- Stall Speed
- Load Factor
- Breguet Range Equation
- Specific Impulse (Isp)
- Tsiolkovsky Rocket Equation
- Multi-Stage Rocket Staging
- Hohmann Transfer Orbit
- Vis-Viva Orbital Parameters
If AviationCalcs has been useful to you, a coffee goes a long way!
Questions or suggestions? contact@aviationcalcs.netlify.app