Paramotor Weight Calculator

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Paramotor Weight Calculator

Calculate All Up Weight (AUW) & Wing Loading for Powered Paragliding

Your weight fully clothed (without flying gear).
Please enter a valid positive weight.
Dry weight of motor, frame, and harness.
Please enter a valid positive weight.
Amount of fuel (Gasoline density approx 0.75 kg/L).
Please enter a valid positive volume.
Weight of the paraglider wing itself.
Please enter a valid positive weight.
Reserve parachute, helmet, instruments, water, etc.
Please enter a valid positive weight.
Used to calculate Wing Loading. Check your wing manual.
Please enter a valid positive area.

Total Flying Weight (AUW)

0 kg
Wing Loading
0
kg/m²
Fuel Weight
0
kg
Rec. Wing Class
Based on Loading
Formula: AUW = Pilot + Motor + (Fuel Vol × 0.75) + Wing + Gear.
Wing Loading = AUW / Wing Area.

Weight Distribution Breakdown

Wing Loading Reference Table

Pilot Level / Wing Type Typical Loading (kg/m²) Characteristics
Beginner / School 3.0 – 4.0 Slow, stable, forgiving
Intermediate / Sport 4.0 – 5.0 Agile, faster, dynamic
Advanced / Competition 5.0 – 6.5+ Very fast, high energy, demanding
Reference values only. Always consult manufacturer specifications.

What is a Paramotor Weight Calculator?

A paramotor weight calculator is an essential flight planning tool used by Powered Paragliding (PPG) pilots to determine their "All Up Weight" (AUW). AUW is the total weight of everything that leaves the ground: the pilot, the motor unit, fuel, the wing itself, and all accessories like a reserve parachute, helmet, and instruments.

Knowing your exact AUW is critical for safety. It determines which wing size you should fly, how your glider will perform, your takeoff speed, and your fuel economy. Many beginners underestimate their total weight, leading to the purchase of undersized wings that can be dangerous to launch and land. This calculator helps eliminate the guesswork by aggregating all component weights into a precise total.

Paramotor Weight Calculator Formula

The calculation for All Up Weight is a summation of all physical components. However, calculating the weight of fuel requires a specific conversion factor because fuel is measured in volume (liters) but contributes to lift requirements in mass (kilograms).

The Mathematical Formula

The core formula used in this tool is:

AUW = Pilot + Motor + (Fuel Volume × Density) + Wing + Accessories

Where:

  • Fuel Density: We use 0.75 kg/L as a standard average for gasoline/oil mixtures used in 2-stroke paramotors.
  • Wing Loading: Calculated as AUW / Wing Area (m²).

Variables Table

Variable Meaning Unit Typical Range
Pilot Weight Body weight clothed kg 50 – 120 kg
Motor Unit Engine, frame, harness kg 20 – 35 kg
Fuel Weight Mass of gas/oil mix kg 0.75 kg per Liter
Wing Loading Weight per square meter kg/m² 3.5 – 6.0 kg/m²
Key variables affecting paramotor flight physics.

Practical Examples (Real-World Use Cases)

Example 1: The Recreational Pilot

John is a recreational pilot weighing 85kg. He flies a reliable Moster 185 unit (27kg) and carries 10 liters of fuel for a morning cross-country flight. He wears a standard helmet and carries a reserve (5kg total gear). His wing weighs 5.5kg.

  • Inputs: Pilot (85), Motor (27), Fuel (10L), Gear (5), Wing (5.5).
  • Fuel Weight: 10L × 0.75 = 7.5kg.
  • Total AUW: 85 + 27 + 7.5 + 5 + 5.5 = 130 kg.
  • Analysis: If John flies a 26m² wing, his loading is 5.0 kg/m², putting him in a sporty/intermediate range.

Example 2: The Light Adventure Pilot

Sarah is a lighter pilot (60kg) using a lightweight titanium frame unit (20kg). She only carries 5 liters of fuel for a quick sunset flight and minimal gear (3kg). Her lightweight mountain wing weighs 4kg.

  • Inputs: Pilot (60), Motor (20), Fuel (5L), Gear (3), Wing (4).
  • Fuel Weight: 5L × 0.75 = 3.75kg.
  • Total AUW: 60 + 20 + 3.75 + 3 + 4 = 90.75 kg.
  • Analysis: Sarah needs a much smaller wing than John. A 20m² wing would give her a loading of ~4.5 kg/m², ideal for stability and agility.

How to Use This Paramotor Weight Calculator

  1. Enter Pilot Weight: Input your body weight. It is best to weigh yourself while wearing your flying clothes and boots.
  2. Enter Motor Weight: Input the "dry weight" of your paramotor (without fuel). Check your manufacturer's manual.
  3. Input Fuel Volume: Enter how many liters of fuel you plan to carry. The calculator automatically converts this to kilograms.
  4. Add Gear & Wing: Don't forget the weight of the glider itself (usually 4-6kg) and your reserve parachute/helmet.
  5. Review Wing Loading: Enter your wing's projected area to see your wing loading. Compare this against the "Wing Loading Reference Table" to ensure you are within the safe range for your skill level.

Key Factors That Affect Paramotor Weight Results

Understanding the nuances of weight in aviation is crucial. Here are six factors that influence your calculations:

  • Fuel Density Variations: While we use 0.75 kg/L, temperature affects fuel density. Cold fuel is denser and heavier than warm fuel.
  • Wing Size vs. Projected Area: Manufacturers list "flat area" and "projected area." Always use projected area for accurate lift calculations, though flat area is often used for general marketing comparisons.
  • Altitude (Density Altitude): While altitude doesn't change your physical weight (mass), it affects lift. At high altitudes, air is thinner, so a specific AUW will feel "heavier" to the wing, requiring a faster takeoff run.
  • Equipment Upgrades: Adding a larger fuel tank, electric start (battery weight), or a heavy reserve parachute can creep up your AUW significantly over time.
  • Thrust-to-Weight Ratio: A higher AUW requires more thrust to climb. If your motor produces 60kg of thrust and your AUW is 130kg, your climb rate will be modest.
  • Structural Limits: Every wing has a certified weight range (e.g., 80-105kg). Flying above this weight (overloading) voids certification and can make the wing react violently to collapses.

Frequently Asked Questions (FAQ)

Does fuel weight really matter for short flights?

Yes. Even 5 liters of fuel weighs nearly 4kg. On a light setup, this is a significant percentage of the total unit weight and affects the center of gravity and takeoff ease.

What happens if my wing loading is too high?

High wing loading increases your stall speed, takeoff speed, and landing speed. The wing becomes more dynamic and reacts faster to inputs, which can be dangerous for beginners.

What happens if my wing loading is too low?

If you are too light for a wing, it becomes sluggish and prone to collapses in turbulence because there isn't enough internal pressure keeping the wing rigid.

Should I include the weight of the paramotor bag?

No, only include items that fly with you. Do not include transport bags or covers left in the car.

How accurate is the 0.75 kg/L fuel estimate?

It is accurate enough for aviation planning. Gasoline is roughly 0.72-0.74 kg/L, and 2-stroke oil is roughly 0.85-0.90 kg/L. The mixture averages out close to 0.75 kg/L.

Does pilot weight include clothes?

Yes. Winter flying suits, heavy boots, and heated gloves can add 3-5kg easily. Always weigh yourself fully dressed for accuracy.

Is AUW the same as "Clip-in Weight"?

Clip-in weight usually refers to the pilot + harness + clothes (everything hooked to the risers). AUW includes the wing itself. Be careful which metric your wing manufacturer uses.

Can I use this for free-flight paragliding?

Yes, simply set the "Motor Weight" and "Fuel" to zero. The logic for AUW and wing loading remains the same.

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Always consult your instructor and equipment manual before flying.

// Initialize calculator on load window.onload = function() { calculateParamotorWeight(); }; function calculateParamotorWeight() { // 1. Get Inputs var pilot = parseFloat(document.getElementById('pilotWeight').value); var motor = parseFloat(document.getElementById('motorWeight').value); var fuelVol = parseFloat(document.getElementById('fuelVolume').value); var wing = parseFloat(document.getElementById('wingWeight').value); var gear = parseFloat(document.getElementById('gearWeight').value); var area = parseFloat(document.getElementById('wingArea').value); // 2. Validation var isValid = true; if (isNaN(pilot) || pilot < 0) { document.getElementById('err-pilot').style.display = 'block'; isValid = false; } else { document.getElementById('err-pilot').style.display = 'none'; } if (isNaN(motor) || motor < 0) { document.getElementById('err-motor').style.display = 'block'; isValid = false; } else { document.getElementById('err-motor').style.display = 'none'; } if (isNaN(fuelVol) || fuelVol < 0) { document.getElementById('err-fuel').style.display = 'block'; isValid = false; } else { document.getElementById('err-fuel').style.display = 'none'; } if (isNaN(wing) || wing < 0) { document.getElementById('err-wing').style.display = 'block'; isValid = false; } else { document.getElementById('err-wing').style.display = 'none'; } if (isNaN(gear) || gear < 0) { document.getElementById('err-gear').style.display = 'block'; isValid = false; } else { document.getElementById('err-gear').style.display = 'none'; } if (isNaN(area) || area 0) { loading = auw / area; } // 4. Determine Class var wingClass = "Unknown"; if (loading = 3.0 && loading = 4.0 && loading = 5.2 && loading = 6.5) wingClass = "Competition / Overloaded"; // 5. Update UI document.getElementById('resultAUW').innerText = auw.toFixed(1); document.getElementById('resultLoading').innerText = loading.toFixed(2); document.getElementById('resultFuelWeight').innerText = fuelWeight.toFixed(1); document.getElementById('resultClass').innerText = wingClass; // 6. Update Chart drawChart(pilot, motor, fuelWeight, wing, gear); } function drawChart(pilot, motor, fuel, wing, gear) { var canvas = document.getElementById('weightChart'); if (!canvas.getContext) return; var ctx = canvas.getContext('2d'); var width = canvas.width; var height = canvas.height; var radius = Math.min(width, height) / 2 – 10; var centerX = width / 2; var centerY = height / 2; var data = [pilot, motor, fuel, wing, gear]; var labels = ["Pilot", "Motor", "Fuel", "Wing", "Gear"]; var colors = ["#004a99", "#28a745", "#ffc107", "#17a2b8", "#6c757d"]; var total = data.reduce(function(a, b) { return a + b; }, 0); ctx.clearRect(0, 0, width, height); var startAngle = 0; for (var i = 0; i < data.length; i++) { if (data[i] <= 0) continue; var sliceAngle = (data[i] / total) * 2 * Math.PI; ctx.beginPath(); ctx.moveTo(centerX, centerY); ctx.arc(centerX, centerY, radius, startAngle, startAngle + sliceAngle); ctx.closePath(); ctx.fillStyle = colors[i]; ctx.fill(); startAngle += sliceAngle; } // Draw Legend // Simple legend drawing on the right or bottom would be complex in pure JS canvas without library // Instead, we will draw a white circle in middle for donut effect and text ctx.beginPath(); ctx.arc(centerX, centerY, radius * 0.5, 0, 2 * Math.PI); ctx.fillStyle = "#ffffff"; ctx.fill(); ctx.fillStyle = "#333"; ctx.font = "bold 16px Arial"; ctx.textAlign = "center"; ctx.textBaseline = "middle"; ctx.fillText("Total", centerX, centerY – 10); ctx.fillText(total.toFixed(1) + " kg", centerX, centerY + 10); } function resetCalculator() { document.getElementById('pilotWeight').value = 80; document.getElementById('motorWeight').value = 27; document.getElementById('fuelVolume').value = 10; document.getElementById('wingWeight').value = 5.5; document.getElementById('gearWeight').value = 4; document.getElementById('wingArea').value = 24; calculateParamotorWeight(); } function copyResults() { var auw = document.getElementById('resultAUW').innerText; var loading = document.getElementById('resultLoading').innerText; var fuelW = document.getElementById('resultFuelWeight').innerText; var wClass = document.getElementById('resultClass').innerText; var text = "Paramotor Weight Calculation:\n"; text += "—————————–\n"; text += "Total All Up Weight (AUW): " + auw + " kg\n"; text += "Wing Loading: " + loading + " kg/m²\n"; text += "Fuel Weight: " + fuelW + " kg\n"; text += "Wing Class Estimate: " + wClass + "\n"; text += "—————————–\n"; text += "Generated by Paramotor Weight Calculator"; var tempInput = document.createElement("textarea"); tempInput.value = text; document.body.appendChild(tempInput); tempInput.select(); document.execCommand("copy"); document.body.removeChild(tempInput); var btn = document.querySelector('.btn-copy'); var originalText = btn.innerText; btn.innerText = "Copied!"; setTimeout(function(){ btn.innerText = originalText; }, 2000); }

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