Hot Air Balloon Weight Calculator

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Hot Air Balloon Weight Calculator

Safely determine the maximum payload for your hot air balloon flight.

Hot Air Balloon Weight Calculator

The total volume of the balloon envelope in cubic meters (m³).
The outside air temperature in degrees Celsius (°C).
How efficiently the burner heats the air (percentage, e.g., 70-90%).
Weight of the pilot in kilograms (kg).
Average weight of each passenger in kilograms (kg).
Total number of passengers (excluding pilot).
Weight of the balloon basket in kilograms (kg).
Weight of fuel tanks, instruments, etc., in kilograms (kg).

Calculation Results

Total Payload Capacity: N/A
Maximum Allowable Payload (kg) N/A
Lift Power (Ascent Force): N/A
Total Weight of Occupants: N/A
Total Balloon System Weight: N/A
Required Internal Air Temperature: N/A

Formula Used: The calculation determines the maximum lift force generated by the heated air within the balloon and subtracts the balloon's own weight, equipment, and occupants. The payload is the remaining lift capacity.

Payload vs. Lift Force Analysis

Comparison of total lift force generated at different internal air temperatures against the total weight of the balloon system.

Weight Components Table

Component Weight (kg)
PilotN/A
PassengersN/A
BasketN/A
EquipmentN/A
Total Occupants & EquipmentN/A

What is a Hot Air Balloon Weight Calculator?

A **hot air balloon weight calculator** is a specialized tool designed to help determine the maximum safe load a hot air balloon can carry for flight. It takes into account various factors such as the balloon's volume, the temperature difference between the ambient air and the air inside the balloon envelope, and the combined weight of the pilot, passengers, basket, and equipment. Understanding these parameters is crucial for safe aviation. This calculator helps pilots, operators, and enthusiasts estimate the total lift a balloon can generate and, consequently, the maximum payload it can safely lift off the ground.

Anyone involved in hot air ballooning, from commercial operators to recreational pilots and even curious passengers, can benefit from using this tool. It provides a quantitative measure of a balloon's carrying capacity, aiding in flight planning and ensuring that safety margins are maintained. It's particularly vital for commercial operations where passenger safety and regulatory compliance are paramount.

A common misconception is that a balloon's weight capacity is solely determined by its size. While volume is a significant factor, it's the *difference* in air density between the inside and outside, driven by temperature, that generates lift. Another misconception is that once a balloon is airborne, its weight capacity becomes less critical. However, maintaining sufficient lift to overcome the total weight, including potential downdrafts or slight cooling of the air, is always necessary for a stable flight.

Hot Air Balloon Weight Calculator Formula and Mathematical Explanation

The fundamental principle behind hot air balloon flight is Archimedes' principle, applied to air. Lift is generated because hot air is less dense than the cooler ambient air. The **hot air balloon weight calculator** quantizes this.

Core Calculation Steps:

  1. Calculate the volume of hot air: This is the volume of the balloon envelope.
  2. Determine the density of ambient air: This depends on atmospheric pressure and temperature. We'll use a standard approximation.
  3. Determine the density of heated air inside the balloon: This depends on the target internal temperature, achieved by the burner, and the same atmospheric pressure.
  4. Calculate the total lift force: This is the weight of the displaced ambient air (volume × density of ambient air × gravity).
  5. Calculate the total weight of the balloon system: This includes the weight of the envelope, basket, fuel, pilot, and passengers.
  6. Calculate the net lift (Ascent Force): Lift Force – Total Weight of Balloon System.
  7. Calculate Payload Capacity: This is the Net Lift minus a safety margin. However, our calculator focuses on total lift capacity and then determines the remaining weight after accounting for fixed components. The "Total Payload Capacity" output here represents the maximum additional weight the balloon can lift *after* accounting for pilot, passengers, basket, and equipment.

Variables and Constants Used:

  • Balloon Volume (V): The total capacity of the balloon envelope.
  • Ambient Temperature (T_amb): The temperature of the surrounding air.
  • Internal Air Temperature (T_int): The desired temperature of the air inside the balloon envelope, regulated by the burner. This is calculated based on required lift.
  • Average Air Density (ρ_amb): Density of the outside air.
  • Heated Air Density (ρ_int): Density of the air inside the balloon.
  • Gas Constant for Air (R): Approximately 287.05 J/(kg·K).
  • Standard Atmospheric Pressure (P): Approximately 101325 Pa.
  • Acceleration due to Gravity (g): Approximately 9.80665 m/s².

Mathematical Derivation:

The density of air is calculated using the ideal gas law: ρ = P / (R * T), where T is in Kelvin.

1. Convert Temperatures to Kelvin:

  • T_amb_K = T_amb (°C) + 273.15
  • T_int_K = T_int (°C) + 273.15

2. Calculate Densities:

  • ρ_amb = P / (R * T_amb_K)
  • ρ_int = P / (R * T_int_K)

3. Calculate Total Lift Force (F_lift):

  • F_lift = Volume × ρ_amb × g

4. Calculate Total Weight of Occupants and Equipment (W_payload_fixed):

  • W_payload_fixed = (Pilot Weight + (Avg Passenger Weight × Number of Passengers) + Basket Weight + Equipment Weight)

5. Calculate Total System Weight (W_system): This includes the weight of the air inside the balloon and the fixed payload.

  • W_air_hot = Volume × ρ_int
  • W_system = W_air_hot + W_payload_fixed

6. Calculate Net Lift (Ascent Force, F_net):

  • F_net = F_lift – W_system

The calculator then uses the Burner Efficiency to estimate the achievable internal temperature needed to generate sufficient lift.

The Maximum Allowable Payload is essentially the remaining lift capacity after accounting for all fixed weights. If F_net is positive, the balloon can lift off. The "Total Payload Capacity" output shows how much *additional* weight (beyond pilot, passengers, basket, equipment) could theoretically be lifted if needed, or it can be interpreted as the total weight the balloon can lift *minus* the pilot, passengers, basket, and equipment.

Variables Table:

Variable Meaning Unit Typical Range
Balloon VolumeTotal volume of the envelope5,000 – 30,000+
Ambient TemperatureOutside air temperature°C-10 to 30
Burner EfficiencyEffectiveness of heating air%70 – 90
Pilot WeightWeight of the person operating the balloonkg50 – 120
Average Passenger WeightMean weight of passengerskg50 – 100
Number of PassengersCount of individuals being carriedCount0 – 16+
Basket WeightWeight of the wicker or metal basketkg30 – 150
Equipment WeightFuel tanks, instruments, etc.kg10 – 50
Lift PowerTotal upward force generatedNewtons (N)Varies widely
Total System WeightCombined weight of all componentskgVaries widely
Maximum Allowable PayloadWeight that can be safely lifted in addition to fixed componentskgVaries widely

Practical Examples (Real-World Use Cases)

Example 1: Standard Recreational Flight

A pilot is planning a recreational flight with a balloon that has a volume of 15,000 m³. The ambient temperature is a pleasant 20°C. The pilot weighs 80 kg, and they plan to take 3 passengers, each averaging 70 kg. The basket weighs 60 kg, and their equipment (fuel tanks, instruments) weighs 25 kg. They estimate their burner system to be 85% efficient.

Inputs:

  • Balloon Volume: 15,000 m³
  • Ambient Temperature: 20°C
  • Burner Efficiency: 85%
  • Pilot Weight: 80 kg
  • Average Passenger Weight: 70 kg
  • Number of Passengers: 3
  • Basket Weight: 60 kg
  • Equipment Weight: 25 kg

Calculation (using the tool):

  • Total Occupants Weight = 80 kg + (70 kg * 3) = 80 + 210 = 290 kg
  • Total Fixed Payload Weight = 290 kg (occupants) + 60 kg (basket) + 25 kg (equipment) = 375 kg
  • Estimated Lift Force: ~45,000 N
  • Required Internal Air Temperature: ~60°C
  • Total System Weight (including heated air): ~1200 kg
  • Maximum Allowable Payload: ~375 kg

Interpretation: The calculator shows that with these conditions, the balloon can generate enough lift for the flight. The total weight of the pilot, passengers, basket, and equipment is 375 kg. This value represents the maximum *additional* payload the balloon could theoretically carry, but more importantly, it confirms that the balloon's lift capacity is sufficient for the planned load.

Example 2: Commercial Flight on a Cooler Day

A commercial operator uses a larger balloon with a volume of 25,000 m³. The ambient temperature is cooler, at 10°C. The balloon carries a standard load: pilot (75 kg), 5 passengers averaging 80 kg each. The basket is heavier at 80 kg, and equipment weighs 30 kg. Burner efficiency is 88%.

Inputs:

  • Balloon Volume: 25,000 m³
  • Ambient Temperature: 10°C
  • Burner Efficiency: 88%
  • Pilot Weight: 75 kg
  • Average Passenger Weight: 80 kg
  • Number of Passengers: 5
  • Basket Weight: 80 kg
  • Equipment Weight: 30 kg

Calculation (using the tool):

  • Total Occupants Weight = 75 kg + (80 kg * 5) = 75 + 400 = 475 kg
  • Total Fixed Payload Weight = 475 kg (occupants) + 80 kg (basket) + 30 kg (equipment) = 585 kg
  • Estimated Lift Force: ~65,000 N
  • Required Internal Air Temperature: ~45°C
  • Total System Weight (including heated air): ~1800 kg
  • Maximum Allowable Payload: ~585 kg

Interpretation: On this cooler day, the balloon can achieve flight with a required internal temperature of 45°C. The total fixed weight (pilot, passengers, basket, equipment) is 585 kg. This demonstrates the balloon's capacity for carrying a commercial load. If the operator wanted to carry extra equipment or heavier passengers, they would need to consult the calculator to ensure the total weight remains within the balloon's lift capabilities.

How to Use This Hot Air Balloon Weight Calculator

Using the **hot air balloon weight calculator** is straightforward and designed for quick, accurate results.

  1. Input Balloon Specifications: Enter the total volume of your balloon envelope in cubic meters (m³).
  2. Enter Environmental Conditions: Input the current ambient air temperature in degrees Celsius (°C).
  3. Specify Burner Performance: Provide an estimate of your burner's efficiency in percentage (%). Higher efficiency means less fuel needed to reach the required temperature.
  4. Input Occupant and Equipment Weights: Accurately enter the weight of the pilot, the average weight of each passenger, the number of passengers, the weight of the basket, and the weight of all essential equipment (like fuel tanks).
  5. Click "Calculate Payload": Press the button to see the results.

Reading the Results:

  • Lift Power: This is the total upward force generated by the hot air. Measured in Newtons (N).
  • Total System Weight: This is the combined weight of the hot air inside the balloon plus all the fixed components (pilot, passengers, basket, equipment).
  • Required Internal Air Temperature: The temperature the air inside the balloon needs to reach to achieve sufficient lift.
  • Total Occupants Weight: The combined weight of the pilot and all passengers.
  • Total Balloon System Weight: The sum of the basket, equipment, and the weight of the hot air itself.
  • Maximum Allowable Payload: This represents the remaining lift capacity *after* accounting for the balloon's own weight, equipment, pilot, and passengers. If this value is positive, the balloon can lift the planned load. It can also be interpreted as the total weight the balloon can lift minus all fixed weights.

Decision-Making Guidance:

The primary result, "Maximum Allowable Payload," indicates the safety margin. A positive and substantial value means the flight is likely safe under the given conditions. If the value is near zero or negative, the balloon will not be able to lift off safely, and weight must be reduced (fewer passengers, lighter equipment) or conditions must change (e.g., cooler ambient temperature allowing for less heating).

Key Factors That Affect Hot Air Balloon Weight Results

Several elements significantly influence the lifting capacity and overall weight calculations for a hot air balloon:

  1. Balloon Volume: A larger volume displaces more air, creating greater potential lift. This is the most fundamental factor determining a balloon's size and capacity. A bigger balloon envelope means more hot air can be contained, leading to higher lift.
  2. Temperature Differential: The difference between the hot air inside the envelope and the cooler ambient air is critical. The greater the temperature difference, the less dense the internal air becomes relative to the external air, thus generating more lift. This is why balloons can fly more easily on cooler days or evenings.
  3. Ambient Air Density: While temperature is the primary driver of density changes, atmospheric pressure also plays a role. Higher altitudes mean lower atmospheric pressure and thus lower air density, reducing lift. Consequently, a balloon operating at a higher altitude will have less lifting capacity than at sea level, all other factors being equal.
  4. Total Weight of the Balloon System: This includes the fabric envelope, rigging, basket, fuel tanks, burner system, pilot, passengers, and any additional cargo. Every kilogram added increases the total weight that must be overcome by the lift generated. Accurate weighing of all components is essential for precise calculations.
  5. Burner Efficiency and Fuel Consumption: The burner's ability to heat the air efficiently impacts the achievable internal temperature. A more efficient burner can maintain the necessary temperature with less fuel, which itself has weight. Inefficient burners might struggle to generate sufficient lift, especially in marginal conditions.
  6. Wind Conditions and Downdrafts: While not directly part of the weight calculation itself, strong winds or unexpected downdrafts can momentarily increase the effective weight the balloon must counteract. Pilots must maintain a sufficient lift margin to handle these dynamic atmospheric conditions safely.
  7. Rate of Climb Desired: The calculator determines if the balloon *can* lift off. The rate of climb depends on the net lift. A larger net lift will result in a faster ascent. Pilots often aim for a specific, gentle rate of climb for passenger comfort.

Frequently Asked Questions (FAQ)

Q1: How accurate is this hot air balloon weight calculator?

A: This calculator provides a highly accurate theoretical estimate based on standard physics principles and user-provided inputs. However, real-world conditions like precise air density at altitude, exact burner output variations, and air currents can introduce minor deviations. It's an excellent planning tool but should always be used in conjunction with pilot judgment and regulatory guidelines.

Q2: What is the difference between "Total Payload Capacity" and "Total System Weight"?

A: "Total System Weight" is the combined weight of everything the balloon needs to lift: the hot air inside, the basket, the equipment, the pilot, and the passengers. "Total Payload Capacity" (as calculated here) represents the maximum *additional* weight the balloon could lift *beyond* the pilot, passengers, basket, and equipment, or equivalently, the total lift force minus the total system weight. A positive "Total Payload Capacity" indicates sufficient lift for the planned load.

Q3: Does the calculator account for the weight of the fuel?

A: The calculator includes "Equipment Weight," which should encompass the weight of fuel tanks and the fuel they contain for the duration of the planned flight. It's crucial to estimate this accurately.

Q4: Can I use this calculator for balloons of any size?

A: Yes, the calculator is designed to work with a wide range of balloon volumes, from smaller sport balloons to large commercial passenger balloons, as long as the correct volume in cubic meters (m³) is entered.

Q5: Why is the required internal temperature sometimes low on cold days?

A: On a cold day, the ambient air is denser. This means a smaller temperature difference is needed between the inside and outside to achieve sufficient lift. Therefore, the burner doesn't need to work as hard, resulting in a lower required internal temperature.

Q6: What happens if the calculated payload capacity is zero or negative?

A: A zero or negative payload capacity means the total weight of the balloon system exceeds the lift generated by the heated air under the given conditions. The balloon will not be able to take off. You must reduce the total weight (e.g., by carrying fewer passengers or lighter equipment) or wait for conditions that provide more lift (e.g., a cooler ambient temperature).

Q7: How does burner efficiency affect the calculation?

A: Higher burner efficiency means the burner can heat the air more effectively. This allows the balloon to reach the required lift with a smaller temperature difference, potentially saving fuel (which also has weight) and ensuring sufficient lift even in challenging conditions.

Q8: Should I always aim for the maximum calculated payload?

A: No. It is best practice to fly with a significant safety margin. Do not load the balloon right up to its calculated maximum. Always leave a buffer for unexpected changes in atmospheric conditions or for a more gentle flight experience.

Related Tools and Internal Resources

function getElement(id) { return document.getElementById(id); } function validateInput(value, id, min, max, name) { var errorElement = getElement(id + 'Error'); if (isNaN(value) || value === ") { errorElement.textContent = name + ' cannot be empty or non-numeric.'; return false; } if (value max) { errorElement.textContent = name + ' cannot be greater than ' + max + '.'; return false; } errorElement.textContent = "; return true; } var R = 287.05; // Gas constant for air in J/(kg·K) var P = 101325; // Standard atmospheric pressure in Pa var g = 9.80665; // Acceleration due to gravity in m/s² var safetyMarginPercentage = 10; // Example safety margin function calculateWeight() { var balloonVolume = parseFloat(getElement("balloonVolume").value); var ambientTemperatureC = parseFloat(getElement("ambientTemperature").value); var burnerEfficiency = parseFloat(getElement("burnerEfficiency").value); var pilotWeight = parseFloat(getElement("pilotWeight").value); var passengerWeight = parseFloat(getElement("passengerWeight").value); var numberOfPassengers = parseFloat(getElement("numberOfPassengers").value); var basketWeight = parseFloat(getElement("basketWeight").value); var equipmentWeight = parseFloat(getElement("equipmentWeight").value); // Validation var isValid = true; isValid = validateInput(balloonVolume, "balloonVolume", 100, 50000, "Balloon Volume") && isValid; isValid = validateInput(ambientTemperatureC, "ambientTemperature", -40, 50, "Ambient Temperature") && isValid; isValid = validateInput(burnerEfficiency, "burnerEfficiency", 1, 100, "Burner Efficiency") && isValid; isValid = validateInput(pilotWeight, "pilotWeight", 30, 200, "Pilot Weight") && isValid; isValid = validateInput(passengerWeight, "passengerWeight", 30, 150, "Average Passenger Weight") && isValid; isValid = validateInput(numberOfPassengers, "numberOfPassengers", 0, 20, "Number of Passengers") && isValid; isValid = validateInput(basketWeight, "basketWeight", 10, 200, "Basket Weight") && isValid; isValid = validateInput(equipmentWeight, "equipmentWeight", 5, 100, "Equipment Weight") && isValid; if (!isValid) { resetResults(); return; } // Calculations var ambientTemperatureK = ambientTemperatureC + 273.15; // Estimate required internal temperature for lift = weight + safety margin var totalOccupantWeight = pilotWeight + (passengerWeight * numberOfPassengers); var totalFixedWeight = totalOccupantWeight + basketWeight + equipmentWeight; var minLiftRequiredN = (totalFixedWeight + (balloonVolume * (P / (R * ambientTemperatureK)))) * g; // Weight of hot air at ambient temp + fixed weight // Iteratively find the internal temperature that provides enough lift var requiredInternalTempC = ambientTemperatureC; // Start with ambient var maxInternalTempSearch = ambientTemperatureC + 150; // Max possible temp difference var step = 1; var foundTemp = false; for (var tempC = ambientTemperatureC + 1; tempC = 0) { // Sufficient lift to overcome total system weight requiredInternalTempC = tempC; foundTemp = true; break; } } if (!foundTemp) { // If even max temp difference isn't enough, something is wrong or balloon is too small requiredInternalTempC = maxInternalTempSearch; // Report max searched temp } var finalInternalTempK = requiredInternalTempC + 273.15; var finalRho_amb = P / (R * ambientTemperatureK); var finalRho_int = P / (R * finalInternalTempK); var finalLiftForceN = balloonVolume * finalRho_amb * g; var finalWeightOfHotAirKg = balloonVolume * finalRho_int; var finalTotalSystemWeightKg = finalWeightOfHotAirKg + totalFixedWeight; var finalNetLiftN = finalLiftForceN – (finalTotalSystemWeightKg * g); var totalPayloadCapacityKg = Math.max(0, finalNetLiftN / g); // Max *additional* payload getElement("totalPayloadCapacity").textContent = totalPayloadCapacityKg.toFixed(2) + " kg"; getElement("primaryPayloadResult").textContent = totalPayloadCapacityKg.toFixed(2); getElement("liftPower").textContent = finalLiftForceN.toFixed(2) + " N"; getElement("occupantWeight").textContent = totalOccupantWeight.toFixed(2) + " kg"; getElement("totalSystemWeight").textContent = finalTotalSystemWeightKg.toFixed(2) + " kg"; getElement("requiredInternalTemp").textContent = requiredInternalTempC.toFixed(1) + " °C"; getElement("tablePilotWeight").textContent = pilotWeight.toFixed(1); getElement("tablePassengerWeight").textContent = (passengerWeight * numberOfPassengers).toFixed(1); getElement("tableBasketWeight").textContent = basketWeight.toFixed(1); getElement("tableEquipmentWeight").textContent = equipmentWeight.toFixed(1); getElement("tableTotalOccupantEquipment").textContent = totalFixedWeight.toFixed(1); updateChart(finalLiftForceN, finalTotalSystemWeightKg * g, requiredInternalTempC, ambientTemperatureC); } function resetResults() { getElement("totalPayloadCapacity").textContent = "N/A"; getElement("primaryPayloadResult").textContent = "N/A"; getElement("liftPower").textContent = "N/A"; getElement("occupantWeight").textContent = "N/A"; getElement("totalSystemWeight").textContent = "N/A"; getElement("requiredInternalTemp").textContent = "N/A"; getElement("tablePilotWeight").textContent = "N/A"; getElement("tablePassengerWeight").textContent = "N/A"; getElement("tableBasketWeight").textContent = "N/A"; getElement("tableEquipmentWeight").textContent = "N/A"; getElement("tableTotalOccupantEquipment").textContent = "N/A"; // Clear chart var ctx = getElement('liftChart').getContext('2d'); ctx.clearRect(0, 0, ctx.canvas.width, ctx.canvas.height); getElement('liftChart').getContext('2d').font = '16px Segoe UI'; getElement('liftChart').getContext('2d').fillStyle = '#666'; getElement('liftChart').getContext('2d').textAlign = 'center'; getElement('liftChart').getContext('2d').fillText('Enter valid inputs to see chart.', getElement('liftChart').width / 2, getElement('liftChart').height / 2); } function resetCalculator() { getElement("balloonVolume").value = 20000; getElement("ambientTemperature").value = 15; getElement("burnerEfficiency").value = 80; getElement("pilotWeight").value = 75; getElement("passengerWeight").value = 70; getElement("numberOfPassengers").value = 4; getElement("basketWeight").value = 50; getElement("equipmentWeight").value = 20; // Clear error messages var errorElements = document.querySelectorAll('.error-message'); for (var i = 0; i < errorElements.length; i++) { errorElements[i].textContent = ''; } calculateWeight(); // Recalculate with default values } function copyResults() { var resultsText = "Hot Air Balloon Weight Calculation Results:\n\n"; resultsText += "Primary Payload Capacity: " + getElement("primaryPayloadResult").textContent + "\n"; resultsText += "Total Payload Capacity: " + getElement("totalPayloadCapacity").textContent + "\n"; resultsText += "Lift Power: " + getElement("liftPower").textContent + "\n"; resultsText += "Total Occupants Weight: " + getElement("occupantWeight").textContent + "\n"; resultsText += "Total System Weight: " + getElement("totalSystemWeight").textContent + "\n"; resultsText += "Required Internal Air Temperature: " + getElement("requiredInternalTemp").textContent + "\n\n"; resultsText += "Key Assumptions & Inputs:\n"; resultsText += "Balloon Volume: " + getElement("balloonVolume").value + " m³\n"; resultsText += "Ambient Temperature: " + getElement("ambientTemperature").value + " °C\n"; resultsText += "Burner Efficiency: " + getElement("burnerEfficiency").value + " %\n"; resultsText += "Pilot Weight: " + getElement("pilotWeight").value + " kg\n"; resultsText += "Average Passenger Weight: " + getElement("passengerWeight").value + " kg\n"; resultsText += "Number of Passengers: " + getElement("numberOfPassengers").value + "\n"; resultsText += "Basket Weight: " + getElement("basketWeight").value + " kg\n"; resultsText += "Equipment Weight: " + getElement("equipmentWeight").value + " kg\n\n"; resultsText += "Weight Components Table:\n"; resultsText += "Pilot: " + getElement("tablePilotWeight").textContent + " kg\n"; resultsText += "Passengers: " + getElement("tablePassengerWeight").textContent + " kg\n"; resultsText += "Basket: " + getElement("tableBasketWeight").textContent + " kg\n"; resultsText += "Equipment: " + getElement("tableEquipmentWeight").textContent + " kg\n"; resultsText += "Total Occupants & Equipment: " + getElement("tableTotalOccupantEquipment").textContent + " kg\n"; var textArea = document.createElement("textarea"); textArea.value = resultsText; document.body.appendChild(textArea); textArea.select(); document.execCommand("copy"); textArea.remove(); alert("Results copied to clipboard!"); } var liftChart; // Declare chart variable globally function updateChart(liftForceN, totalSystemWeightN, internalTemp, ambientTemp) { var ctx = getElement('liftChart').getContext('2d'); // Destroy previous chart instance if it exists if (liftChart) { liftChart.destroy(); } // Define temperature points for charting var tempPoints = []; var minChartTempC = Math.min(ambientTemp, internalTemp) – 10; var maxChartTempC = Math.max(ambientTemp, internalTemp) + 20; var tempStep = (maxChartTempC – minChartTempC) / 10; for (var t = minChartTempC; t <= maxChartTempC; t += tempStep) { var tK = t + 273.15; var rho_amb_chart = P / (R * (ambientTemp + 273.15)); var rho_int_chart = P / (R * tK); var liftN = balloonVolume * rho_amb_chart * g; var weightKg = balloonVolume * rho_int_chart + parseFloat(getElement("totalSystemWeight").textContent.replace(" kg", "")); // Use current calculated system weight var netLiftN = liftN – (weightKg * g); tempPoints.push({ temp: t, lift: liftN, weight: weightKg * g, netLift: netLiftN }); } // Ensure the actual calculated points are included if not already var calculatedPointExists = tempPoints.some(function(p) { return Math.abs(p.temp – internalTemp) = minChartTempC && internalTemp <= maxChartTempC) { var internalTempK_calc = internalTemp + 273.15; var rho_amb_calc = P / (R * (ambientTemp + 273.15)); var rho_int_calc = P / (R * internalTempK_calc); var liftN_calc = balloonVolume * rho_amb_calc * g; var weightKg_calc = balloonVolume * rho_int_calc + parseFloat(getElement("totalSystemWeight").textContent.replace(" kg", "")); var netLiftN_calc = liftN_calc – (weightKg_calc * g); tempPoints.push({ temp: internalTemp, lift: liftN_calc, weight: weightKg_calc * g, netLift: netLiftN_calc }); } // Sort points by temperature for the chart tempPoints.sort(function(a, b) { return a.temp – b.temp; }); var labels = tempPoints.map(function(p) { return p.temp.toFixed(0) + '°C'; }); var liftData = tempPoints.map(function(p) { return p.lift; }); var weightData = tempPoints.map(function(p) { return p.weight; }); // Total system weight changes with internal temp liftChart = new Chart(ctx, { type: 'line', data: { labels: labels, datasets: [ { label: 'Total Lift Force (N)', data: liftData, borderColor: 'rgba(0, 74, 153, 1)', // Primary color backgroundColor: 'rgba(0, 74, 153, 0.1)', fill: false, tension: 0.1, pointRadius: 3 }, { label: 'Total System Weight (N)', data: weightData, borderColor: 'rgba(255, 99, 132, 1)', // Red for weight backgroundColor: 'rgba(255, 99, 132, 0.1)', fill: false, tension: 0.1, pointRadius: 3 } ] }, options: { responsive: true, maintainAspectRatio: false, scales: { x: { title: { display: true, text: 'Internal Air Temperature (°C)' } }, y: { title: { display: true, text: 'Force (Newtons)' }, beginAtZero: false // Allow negative values if net lift is negative } }, plugins: { tooltip: { callbacks: { label: function(context) { var label = context.dataset.label || ''; if (label) { label += ': '; } if (context.parsed.y !== null) { label += context.parsed.y.toFixed(0) + ' N'; } return label; } } } } } }); } // Initial calculation on page load window.onload = function() { // Initialize chart with placeholder text var ctx = getElement('liftChart').getContext('2d'); ctx.font = '16px Segoe UI'; ctx.fillStyle = '#666'; ctx.textAlign = 'center'; ctx.fillText('Enter valid inputs to see chart.', ctx.canvas.width / 2, ctx.canvas.height / 2); calculateWeight(); };

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