Ballon Carry Weight Calculation

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Ballon Carry Weight Calculation

Determine the maximum payload your balloon can safely lift with our comprehensive calculator and guide.

Carry Weight Calculator

The total volume of the balloon's envelope.
Helium Hydrogen Hot Air
Select the gas used for lift (Helium, Hydrogen, or Hot Air).
The temperature of the lifting gas inside the balloon.
The temperature of the surrounding air.
The atmospheric pressure at the balloon's altitude (e.g., sea level is 1013.25 hPa).
The weight of the balloon fabric and structure itself.
Weight of gondola, instruments, etc. (excluding passengers/cargo).

Maximum Carry Weight

Calculates maximum carry weight by finding the total lift force and subtracting the balloon's structural weight and any existing payload.

Calculation Details

Lift Force vs. Gas Type
Key Values and Assumptions
Variable Value Unit
Balloon Volume
Lifting Gas
Gas Temperature°C
Ambient Temperature°C
Ambient PressurehPa
Balloon Material Weightkg
Existing Payloadkg

Ballon Carry Weight Calculation: Your Definitive Guide

The ability of a balloon to lift external weight, known as its carry weight or payload capacity, is a critical factor for any aerial application, from recreational hot air ballooning to scientific research and cargo transport. Understanding how to accurately calculate this value ensures safety, efficiency, and operational success. This comprehensive guide delves into the physics behind balloon lift, provides a practical calculator, and explores the key factors influencing a balloon's carrying capacity.

What is Ballon Carry Weight Calculation?

Ballon carry weight calculation is the process of determining the maximum external load (payload) a balloon can lift and sustain in flight. This calculation is fundamentally based on the principle of buoyancy, specifically Archimedes' principle, applied to gases. It involves assessing the lifting force generated by the difference in density between the lifting gas inside the balloon and the ambient air, and then subtracting the balloon's own weight and any fixed equipment. A precise ballon carry weight calculation is essential for aviation safety and operational planning.

Who should use it:

  • Hot air balloon pilots and operators
  • Gas balloonists (helium, hydrogen)
  • Engineers designing lighter-than-air vehicles
  • Hobbyists involved in ballooning projects
  • Event organizers planning aerial promotions

Common misconceptions:

  • "More gas equals more lift." While true to an extent, lift is primarily determined by the *density difference* and the *volume* of the lifting gas, not just the quantity.
  • "Carry weight is fixed." Carry weight varies significantly with ambient temperature, pressure (altitude), and the specific lifting gas used.
  • "It's just about the balloon's volume." The weight of the balloon material, gondola, and any pre-existing equipment are crucial deductions from the gross lifting force.

{primary_keyword} Formula and Mathematical Explanation

The calculation of ballon carry weight revolves around determining the gross lifting force and then subtracting all non-lifting weights. Here's a breakdown:

1. Density of Lifting Gas (ρ_gas):

This depends on the gas type, its temperature, and the ambient pressure. For ideal gases, the ideal gas law is used: PV = nRT, which can be rearranged to density (ρ = m/V). A simplified form is:

ρ_gas = (Molecular Weight * P_gas) / (R_specific * T_absolute)

Where:

  • P_gas is the partial pressure of the gas (often approximated as ambient pressure for a flexible balloon).
  • T_absolute is the absolute temperature (in Kelvin).
  • R_specific is the specific gas constant for the lifting gas.

For simplicity in our calculator, we use standard densities adjusted for temperature and pressure.

2. Density of Ambient Air (ρ_air):

Similar to gas density, it uses the ideal gas law for air.

ρ_air = (Molecular Weight of Air * P_ambient) / (R_specific_air * T_absolute_ambient)

3. Buoyant Force (Lift):

This is the total upward force exerted by the surrounding air on the volume of gas displaced. According to Archimedes' principle:

Buoyant Force = Volume_balloon * ρ_air * g

Where 'g' is the acceleration due to gravity (approx. 9.81 m/s²). This is the force that lifts the entire balloon system.

4. Total Weight of Lifting Gas (W_gas):

W_gas = Volume_balloon * ρ_gas * g

5. Net Lift (Gross Lift):

This is the upward force available to lift the balloon structure and its payload.

Net Lift = Buoyant Force – W_gas

Net Lift = Volume_balloon * (ρ_air – ρ_gas) * g

This can also be expressed as the weight of the displaced air minus the weight of the lifting gas within the balloon.

Our calculator simplifies this to "Gross Lift", which is the total upward force available.

6. Total Weight of the Balloon System:

Total System Weight = Balloon Material Weight + Existing Payload Weight + (Optional: Weight of any passengers/cargo if pre-calculated)

7. Maximum Carry Weight (Payload Capacity):

This is the maximum additional weight the balloon can lift beyond its own structure and existing payload.

Maximum Carry Weight = Net Lift – Balloon Material Weight – Existing Payload Weight

The calculator directly provides "Maximum Carry Weight" by calculating Net Lift and subtracting the given material and payload weights.

Variable Explanations:

Variable Meaning Unit Typical Range
Volume_balloonThe internal volume of the balloon envelope.10 – 100,000+
Lifting Gas TypeThe gas used to generate lift (Helium, Hydrogen, Hot Air).
Gas Temperature (T_gas)Temperature of the lifting gas inside the balloon.°C-50 to 120 (Hot Air) / -20 to 30 (He/H2)
Ambient Temperature (T_air)Temperature of the surrounding air.°C-50 to 40
Ambient Pressure (P_air)Atmospheric pressure at the balloon's altitude.hPa500 – 1013.25
Balloon Material WeightWeight of the fabric, ropes, and structure.kg10 – 5000+
Existing Payload WeightWeight of gondola, instruments, burner system (for HA balloons), etc.kg5 – 2000+
Lift per Cubic MeterThe effective lift generated by each cubic meter of lifting gas.kg/m³~1.1 (Helium) / ~1.2 (Hydrogen) / ~0.3 (Hot Air @ 100°C delta)
Total Lift ForceThe total buoyant force generated by the balloon's volume of gas.kg-force (or N)Varies widely
Gross LiftNet upward force available before subtracting structural weight.kgVaries widely
Maximum Carry WeightThe maximum additional weight the balloon can lift.kgVaries widely

Practical Examples (Real-World Use Cases)

Let's illustrate ballon carry weight calculation with two distinct scenarios:

Example 1: Recreational Hot Air Balloon

A hot air balloon operator is preparing for a morning flight. They need to know how much passenger weight they can safely accommodate.

  • Balloon Volume: 3000 m³
  • Lifting Gas: Hot Air
  • Gas Temperature: 100°C (relative to ambient)
  • Ambient Temperature: 15°C
  • Ambient Pressure: 1013.25 hPa
  • Balloon Material Weight: 150 kg
  • Existing Payload Weight: 70 kg (burner, fuel tanks, basket)

Using the calculator with these inputs:

  • Lift per Cubic Meter: ~0.37 kg/m³ (Hot Air)
  • Total Lift Force: ~1110 kg-force
  • Gross Lift: ~960 kg
  • Maximum Carry Weight: 960 kg – 150 kg – 70 kg = 740 kg

Interpretation: This balloon can carry an additional 740 kg. If the average passenger (plus their belongings) weighs 85 kg, they could accommodate approximately 740 / 85 = 8.7 passengers. Thus, they should limit passenger numbers to 8 for safety.

Example 2: Scientific Research Helium Balloon

A research team is launching a weather monitoring balloon with sensitive equipment.

  • Balloon Volume: 50 m³
  • Lifting Gas: Helium
  • Gas Temperature: 20°C
  • Ambient Temperature: 18°C
  • Ambient Pressure: 980 hPa (higher altitude)
  • Balloon Material Weight: 15 kg
  • Existing Payload Weight: 5 kg (instrument housing, wiring)

Using the calculator:

  • Lift per Cubic Meter: ~1.08 kg/m³ (Helium at these conditions)
  • Total Lift Force: ~54 kg-force
  • Gross Lift: ~53.2 kg
  • Maximum Carry Weight: 53.2 kg – 15 kg – 5 kg = 33.2 kg

Interpretation: The balloon can lift an additional 33.2 kg. This capacity must accommodate all scientific instruments, data loggers, and any ballast needed for altitude control.

How to Use This Ballon Carry Weight Calculator

Our interactive calculator simplifies the complex physics into easy-to-understand inputs and outputs. Follow these steps for an accurate ballon carry weight calculation:

  1. Enter Balloon Volume: Input the total volume of your balloon envelope in cubic meters (m³).
  2. Select Lifting Gas: Choose "Helium", "Hydrogen", or "Hot Air" from the dropdown menu.
  3. Input Temperatures: Enter the temperature of the lifting gas (°C) and the surrounding ambient air (°C). For hot air balloons, the gas temperature is the *operating* temperature, often significantly higher than ambient.
  4. Enter Ambient Pressure: Input the atmospheric pressure in hectopascals (hPa). Sea level is typically 1013.25 hPa; this decreases with altitude.
  5. Enter Weights: Input the weight of the balloon's material (fabric, envelope, rigging) in kg, and the weight of any existing, fixed payload (e.g., basket, burner system) in kg.
  6. Click Calculate: The calculator will instantly display the results.

How to read results:

  • Maximum Carry Weight (Primary Result): This is the total weight of additional items (passengers, cargo, scientific instruments) your balloon can lift.
  • Lift per Cubic Meter: Shows how much weight each cubic meter of your chosen gas provides.
  • Total Lift Force: The total upward force generated by the balloon.
  • Gross Lift: The net upward force available after accounting for the gas's own weight, but before subtracting the balloon's structure.
  • Key Values and Assumptions Table: Provides a summary of your inputs for verification.
  • Chart: Visually compares the lift generated by different gas types under similar conditions (or shows lift variation if only one gas is selected).

Decision-making guidance:

  • Ensure your total desired payload (passengers + cargo) does not exceed the calculated "Maximum Carry Weight".
  • Always maintain a safety margin. Do not operate at the absolute maximum calculated limit.
  • Changes in ambient temperature and altitude (pressure) significantly affect lift. Re-calculate if conditions change drastically.

Key Factors That Affect Ballon Carry Weight Results

Several variables play a crucial role in determining a balloon's lifting capability. Understanding these helps in accurate ballon carry weight calculation and operational adjustments:

  1. Volume of the Balloon: This is the most direct factor. A larger volume displaces more air, leading to greater buoyant force. All else being equal, a bigger balloon lifts more.
  2. Density Difference (Gas vs. Air): The core of buoyancy. A greater difference between the density of the lifting gas and the surrounding air results in higher lift. This is why Helium and Hydrogen provide more lift per volume than hot air.
  3. Temperature of the Lifting Gas: Especially critical for hot air balloons. Heating the air inside the envelope makes it less dense than the cooler ambient air. Higher temperatures create a larger density difference and thus more lift. For gas balloons, temperature variations still affect gas density, though less dramatically than in hot air balloons.
  4. Ambient Air Temperature: Affects the density of the surrounding air. Colder ambient air is denser, increasing buoyant force. This is why balloons often have better lift on cooler mornings.
  5. Altitude (Ambient Pressure): As altitude increases, atmospheric pressure decreases. This lowers the density of the ambient air, reducing the buoyant force and thus the balloon's lifting capacity. Our ballon carry weight calculation needs accurate pressure data for specific altitudes.
  6. Type of Lifting Gas: Helium and Hydrogen are significantly denser than heated air, providing more lift per cubic meter. Hydrogen offers slightly more lift than Helium but comes with significant flammability risks.
  7. Weight of Balloon Structure: The fabric of the envelope, rigging, basket, burner system (for hot air), and any attached equipment all contribute to the total weight that must be lifted. Reducing the weight of these components increases the available carry weight.
  8. Moisture Content: Water vapor is less dense than dry air. High humidity can slightly reduce the lift of a hot air balloon, while the moisture content within the lifting gas itself also affects its density.

Frequently Asked Questions (FAQ)

  • Q1: What is the difference between "Gross Lift" and "Maximum Carry Weight"?
    Gross Lift is the total upward force generated by the balloon. Maximum Carry Weight is the Gross Lift minus the weight of the balloon's structure and any existing payload. It's the weight of *additional* items the balloon can lift.
  • Q2: Does temperature have a bigger impact on Hot Air or Gas Balloons?
    Temperature has a much larger impact on Hot Air Balloons because lift is generated by heating the air significantly above ambient. Gas balloons (Helium, Hydrogen) are affected by temperature changes, but less dramatically, as their lift comes from inherent density difference.
  • Q3: Why is Hydrogen lift slightly higher than Helium?
    Hydrogen has a lower molecular weight (approx. 2 g/mol) than Helium (approx. 4 g/mol). This means a given volume of Hydrogen is less dense than the same volume of Helium at the same temperature and pressure, resulting in slightly greater lift. However, Hydrogen's extreme flammability makes Helium the preferred choice for most applications.
  • Q4: How does altitude affect my balloon's carrying capacity?
    As altitude increases, air density decreases. This means the buoyant force generated by displacing air is reduced. Therefore, a balloon's carrying capacity decreases at higher altitudes. The ballon carry weight calculation needs to account for ambient pressure changes.
  • Q5: Can I use this calculator for weather balloons?
    Yes, provided you input the correct volume, gas type (usually Helium), temperatures, pressure, and the weights of the balloon material and instrumentation payload.
  • Q6: What happens if I exceed the Maximum Carry Weight?
    If the total weight (balloon structure + existing payload + new payload) exceeds the Gross Lift, the balloon will not be able to ascend or will have dangerously little excess lift for controlled flight, posing a significant safety risk.
  • Q7: Does rain or moisture affect lift?
    Yes, moisture adds weight to the balloon envelope and can slightly alter air density. For hot air balloons, accumulated moisture can noticeably reduce performance. It's best to fly in dry conditions for optimal lift.
  • Q8: How often should I recalculate my balloon's carry weight?
    Recalculate if there are significant changes in: ambient temperature, altitude (pressure), gas temperature (for hot air), or if the balloon's structure or fixed payload weight changes. Always check before a flight, especially if conditions differ from standard operating parameters.

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// Constants for gas properties (approximate values) var GAS_PROPERTIES = { helium: { molecularWeight: 4.0026, specificGasConstant: 2077 }, // J/(kg·K) hydrogen: { molecularWeight: 2.016, specificGasConstant: 4157 }, // J/(kg·K) hotair: { molecularWeight: 28.964, specificGasConstant: 287.05 } // J/(kg·K) – for air, adjusted for temperature delta }; var MOLAR_GAS_CONSTANT = 8.314; // J/(mol·K) var GRAVITY = 9.80665; // m/s^2 var STD_PRESSURE = 1013.25; // hPa var STD_TEMP_AIR_CELSIUS = 15; // °C var STD_TEMP_AIR_KELVIN = STD_TEMP_AIR_CELSIUS + 273.15; // K // Default values var DEFAULT_VALUES = { balloonVolume: 100, gasType: 'helium', gasTemperature: 20, ambientTemperature: 15, ambientPressure: 1013.25, balloonMaterialWeight: 50, payloadWeight: 10 }; function kelvinToCelsius(kelvin) { return kelvin – 273.15; } function celsiusToKelvin(celsius) { return celsius + 273.15; } function hPaToPascals(hPa) { return hPa * 100; } function calculateDensity(gasType, temperatureC, pressureHPa) { var tempK = celsiusToKelvin(temperatureC); var pressurePa = hPaToPascals(pressureHPa); var gas = GAS_PROPERTIES[gasType]; if (!gas) return NaN; var density; if (gasType === 'hotair') { // For hot air, we calculate lift based on temperature difference. // The density difference is key. A common approximation for lift per m³: // Lift_kg/m³ ≈ (1.225 * (1 – (GasTempK / AmbientTempK))) * (PressureHPa / 1013.25) // Where 1.225 kg/m³ is standard air density at sea level (15°C, 1013.25 hPa). // Let's derive a more direct density calculation. var ambientDensityStd = (GAS_PROPERTIES.hotair.molecularWeight * STD_PRESSURE) / (GAS_PROPERTIES.hotair.specificGasConstant * STD_TEMP_AIR_KELVIN); // Approx 1.225 kg/m³ var currentAmbientDensity = (GAS_PROPERTIES.hotair.molecularWeight * pressurePa) / (GAS_PROPERTIES.hotair.specificGasConstant * celsiusToKelvin(STD_TEMP_AIR_CELSIUS)); // Density of air at given ambient temp/pressure var gasDensity = (GAS_PROPERTIES.hotair.molecularWeight * pressurePa) / (GAS_PROPERTIES.hotair.specificGasConstant * tempK); // Density of hot air at given temp/pressure // For Hot Air, lift is primarily from the *difference* in density due to temperature. // The "gas density" here represents the density of the heated air. density = gasDensity; } else { // For Helium and Hydrogen var molecularWeight = gas.molecularWeight; density = (molecularWeight * pressurePa) / (MOLAR_GAS_CONSTANT * tempK); } return density; } function getLiftPerCubicMeter(gasType, gasTempC, ambientTempC, ambientPressureHPa) { var ambientDensity = calculateDensity('hotair', ambientTempC, ambientPressureHPa); // Always use standard air density calculation for ambient var gasDensity; if (gasType === 'hotair') { var gasTempK = celsiusToKelvin(gasTempC); var ambientTempK = celsiusToKelvin(ambientTempC); var tempDelta = ambientTempK – gasTempK; // Note: This should be gasTempK – ambientTempK for temperature *increase* var hotAirDensity = calculateDensity('hotair', gasTempC, ambientPressureHPa); // Density of the heated air // Lift is based on the difference in density. If gasTempC is delta *above* ambient, use that. // Simplified: Lift ≈ (Ambient Density) * g * Delta V / V = Ambient Density * g * (1 – rho_gas/rho_air) // A common simplified approach for hot air lift is based on temperature delta: // Lift (kg/m^3) ≈ 0.33 * (Temp_gas_in_C – Temp_ambient_in_C) * (Pressure_hPa / 1013.25) var lift = 0.33 * (gasTempC – ambientTempC) * (ambientPressureHPa / 1013.25); if (lift 0 ? lift : 0; } } function calculateCarryWeight() { // Input validation var inputs = { balloonVolume: parseFloat(document.getElementById('balloonVolume').value), gasType: document.getElementById('gasType').value, gasTemperature: parseFloat(document.getElementById('gasTemperature').value), ambientTemperature: parseFloat(document.getElementById('ambientTemperature').value), ambientPressure: parseFloat(document.getElementById('ambientPressure').value), balloonMaterialWeight: parseFloat(document.getElementById('balloonMaterialWeight').value), payloadWeight: parseFloat(document.getElementById('payloadWeight').value) }; var errors = { balloonVolume: ", gasTypeError: ", gasTemperatureError: ", ambientTemperatureError: ", ambientPressureError: ", balloonMaterialWeightError: ", payloadWeightError: " }; // Numeric input validation if (isNaN(inputs.balloonVolume) || inputs.balloonVolume <= 0) { errors.balloonVolume = 'Please enter a positive volume.'; } if (isNaN(inputs.gasTemperature)) { errors.gasTemperatureError = 'Please enter a valid gas temperature.'; } if (isNaN(inputs.ambientTemperature)) { errors.ambientTemperatureError = 'Please enter a valid ambient temperature.'; } if (isNaN(inputs.ambientPressure) || inputs.ambientPressure <= 0) { errors.ambientPressureError = 'Please enter a positive pressure.'; } if (isNaN(inputs.balloonMaterialWeight) || inputs.balloonMaterialWeight < 0) { errors.balloonMaterialWeightError = 'Material weight cannot be negative.'; } if (isNaN(inputs.payloadWeight) || inputs.payloadWeight < 0) { errors.payloadWeightError = 'Payload weight cannot be negative.'; } // Display errors document.getElementById('balloonVolumeError').innerText = errors.balloonVolume; document.getElementById('gasTypeError').innerText = errors.gasTypeError; // Gas type has no explicit error handling here, assuming valid selection document.getElementById('gasTemperatureError').innerText = errors.gasTemperatureError; document.getElementById('ambientTemperatureError').innerText = errors.ambientTemperatureError; document.getElementById('ambientPressureError').innerText = errors.ambientPressureError; document.getElementById('balloonMaterialWeightError').innerText = errors.balloonMaterialWeightError; document.getElementById('payloadWeightError').innerText = errors.payloadWeightError; if (errors.balloonVolume || errors.gasTemperatureError || errors.ambientTemperatureError || errors.ambientPressureError || errors.balloonMaterialWeightError || errors.payloadWeightError) { document.getElementById('resultsDisplay').style.display = 'none'; return; // Stop calculation if there are errors } var liftPerCubicMeter = getLiftPerCubicMeter( inputs.gasType, inputs.gasTemperature, inputs.ambientTemperature, inputs.ambientPressure ); if (isNaN(liftPerCubicMeter) || liftPerCubicMeter < 0) { document.getElementById('resultsDisplay').style.display = 'none'; // Consider adding a specific error message for calculation issues return; } var totalLiftForce = inputs.balloonVolume * liftPerCubicMeter * GRAVITY; // Force in Newtons var grossLift = inputs.balloonVolume * liftPerCubicMeter; // Mass equivalent in kg var balloonSystemWeight = inputs.balloonMaterialWeight + inputs.payloadWeight; var maxCarryWeight = grossLift – balloonSystemWeight; if (maxCarryWeight 0 ? heliumLift : 0); comparisonData.datasets[0].data.push(hydrogenLift > 0 ? hydrogenLift : 0); comparisonData.datasets[0].data.push(hotAirLift > 0 ? hotAirLift : 0); // Highlight the selected gas's performance var selectedGasIndex = comparisonData.labels.indexOf(selectedGasType.charAt(0).toUpperCase() + selectedGasType.slice(1)); if (selectedGasIndex !== -1) { comparisonData.datasets[0].backgroundColor[selectedGasIndex] = 'rgba(40, 167, 69, 0.8)'; // Success color comparisonData.datasets[0].borderColor[selectedGasIndex] = 'rgba(40, 167, 69, 1)'; } // Ensure the currently calculated value is reflected if it differs significantly from standard // We'll use the calculated value directly for the selected gas if it's not a standard comparison point if (selectedGasType !== 'hotair') { var currentLift = selectedGasLift; // Use the actual calculated lift // Find index for Helium/Hydrogen if they were selected if (selectedGasType === 'helium' && comparisonData.labels[0] === 'Helium') comparisonData.datasets[0].data[0] = currentLift > 0 ? currentLift : 0; if (selectedGasType === 'hydrogen' && comparisonData.labels[1] === 'Hydrogen') comparisonData.datasets[0].data[1] = currentLift > 0 ? currentLift : 0; } // Destroy previous chart instance if it exists var existingChart = Chart.getChart(ctx); if (existingChart) { existingChart.destroy(); } new Chart(ctx, { type: 'bar', data: comparisonData, options: { responsive: true, maintainAspectRatio: false, plugins: { title: { display: true, text: 'Comparative Lift Force by Gas Type', color: 'var(–primary-color)' }, legend: { display: false // Hide legend as colors are explained in caption/data } }, scales: { y: { beginAtZero: true, title: { display: true, text: 'Lift (kg per cubic meter)', color: 'var(–primary-color)' }, ticks: { color: 'var(–text-color)' } }, x: { title: { display: true, text: 'Lifting Gas', color: 'var(–primary-color)' }, ticks: { color: 'var(–text-color)' } } } } }); document.getElementById('chartCaption').innerText = 'Comparison of Lift Force per m³ for different gases. The highlighted bar represents the performance of ' + selectedGasType.charAt(0).toUpperCase() + selectedGasType.slice(1) + ' under calculated conditions.'; } function resetCalculator() { document.getElementById('balloonVolume').value = DEFAULT_VALUES.balloonVolume; document.getElementById('gasType').value = DEFAULT_VALUES.gasType; document.getElementById('gasTemperature').value = DEFAULT_VALUES.gasTemperature; document.getElementById('ambientTemperature').value = DEFAULT_VALUES.ambientTemperature; document.getElementById('ambientPressure').value = DEFAULT_VALUES.ambientPressure; document.getElementById('balloonMaterialWeight').value = DEFAULT_VALUES.balloonMaterialWeight; document.getElementById('payloadWeight').value = DEFAULT_VALUES.payloadWeight; // Clear errors document.getElementById('balloonVolumeError').innerText = "; document.getElementById('gasTypeError').innerText = "; document.getElementById('gasTemperatureError').innerText = "; document.getElementById('ambientTemperatureError').innerText = "; document.getElementById('ambientPressureError').innerText = "; document.getElementById('balloonMaterialWeightError').innerText = "; document.getElementById('payloadWeightError').innerText = "; document.getElementById('resultsDisplay').style.display = 'none'; // Optionally recalculate immediately after reset // calculateCarryWeight(); } function copyResults() { var primaryResult = document.getElementById('primaryResult').innerText; var liftPerCubicMeter = document.getElementById('liftPerCubicMeter').innerText; var totalLiftForce = document.getElementById('totalLiftForce').innerText; var grossLift = document.getElementById('grossLift').innerText; var volValue = document.getElementById('volValue').innerText; var gasValue = document.getElementById('gasValue').innerText; var gasTempVal = document.getElementById('gasTempVal').innerText; var ambTempVal = document.getElementById('ambTempVal').innerText; var ambPressVal = document.getElementById('ambPressVal').innerText; var matWeightVal = document.getElementById('matWeightVal').innerText; var payloadVal = document.getElementById('payloadVal').innerText; var copyText = "— Ballon Carry Weight Calculation Results —\n\n"; copyText += "Primary Result:\n" + primaryResult + "\n\n"; copyText += "Details:\n"; copyText += "- " + liftPerCubicMeter + "\n"; copyText += "- " + totalLiftForce + "\n"; copyText += "- " + grossLift + "\n\n"; copyText += "Key Assumptions:\n"; copyText += "- Balloon Volume: " + volValue + " m³\n"; copyText += "- Lifting Gas: " + gasValue + "\n"; copyText += "- Gas Temperature: " + gasTempVal + " °C\n"; copyText += "- Ambient Temperature: " + ambTempVal + " °C\n"; copyText += "- Ambient Pressure: " + ambPressVal + " hPa\n"; copyText += "- Balloon Material Weight: " + matWeightVal + " kg\n"; copyText += "- Existing Payload: " + payloadVal + " kg\n"; navigator.clipboard.writeText(copyText).then(function() { alert('Results copied to clipboard!'); }, function(err) { console.error('Failed to copy results: ', err); // Fallback for browsers that don't support Clipboard API easily var textArea = document.createElement("textarea"); textArea.value = copyText; textArea.style.position = "fixed"; textArea.style.left = "-9999px"; document.body.appendChild(textArea); textArea.focus(); textArea.select(); try { document.execCommand('copy'); alert('Results copied to clipboard!'); } catch (e) { alert('Could not copy text. Please copy manually.'); console.error('Copy fallback failed: ', e); } document.body.removeChild(textArea); }); } // Initial calculation on page load window.onload = function() { // Ensure Chart.js is loaded before trying to use it if (typeof Chart === 'undefined') { console.error("Chart.js is not loaded. Please include Chart.js library."); document.getElementById('chartContainer').innerHTML = 'Chart could not be loaded. Ensure Chart.js is included.'; return; } calculateCarryWeight(); // Perform initial calculation with default values }; // Add Chart.js library dynamically if not already present. // In a real WordPress environment, you'd enqueue this script properly. if (typeof Chart === 'undefined') { var script = document.createElement('script'); script.src = 'https://cdn.jsdelivr.net/npm/chart.js@4.4.0/dist/chart.umd.min.js'; // Use a specific version script.onload = function() { console.log('Chart.js loaded.'); // Recalculate after Chart.js is loaded if it wasn't already if (typeof Chart !== 'undefined') { calculateCarryWeight(); } }; script.onerror = function() { console.error('Failed to load Chart.js.'); document.getElementById('chartContainer').innerHTML = 'Chart could not be loaded due to network error.'; }; document.head.appendChild(script); } else { console.log('Chart.js already loaded.'); // Ensure the chart is updated if it was rendered before Chart.js fully initialized // calculateCarryWeight(); // This might be redundant if onload handles it }

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