Cryogenic Propellant Boil-Off Calculator

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Why Cryogenic Boil-Off Matters

Liquid hydrogen (LH2) and liquid oxygen (LOX) are core workhorses of high-performance rocket stages, test stands, and long-duration space missions. Their low temperatures and high specific impulse come with a practical challenge: any heat leaking into the tank causes part of the liquid to vaporize, a process known as boil-off.

Even seemingly small heat fluxes (fractions of a watt per square metre) can accumulate over hours or days, leading to significant mass loss, pressure rise, and the need for venting. Accurate boil-off estimates are therefore critical for:

This Cryogenic Propellant Boil-Off Calculator uses a simplified thermal balance model to estimate a volumetric boil-off rate, a storage “half-life” (time until 50% of the tank volume is lost), and a qualitative risk score for rapid loss.

Thermal Balance Model and Formulas

The model assumes a uniform average heat flux q (W/m²) through the tank boundary and a surface area A (m²). The total heat leak rate is

Total heat leak:

Q̇ = q × A   (watts)

Over a period of one hour (3600 s), the energy absorbed by the propellant is

Energy per hour:

Q = Q̇ × 3600   (joules)

If the latent heat of vaporization is Lv (kJ/kg), converted to J/kg as 1000 × Lv, the corresponding mass boiled off per hour ṁ (kg/h) is

Mass boil-off rate:

ṁ = (q × A × 3600) / (1000 × Lv)

Using the liquid density ρ (kg/m³), this is converted to a volumetric boil-off rate V̇ (m³/h):

Volumetric boil-off rate:

V̇ = ṁ / ρ

For a tank with liquid volume V (m³), the time to lose half of that volume, t50, is

Storage half-life (50% loss time):

t50 = (0.5 × V) / V̇

The calculator also provides a logistic-style risk score to express how quickly this 50% loss occurs relative to a one-day (24 h) reference.

Risk score formula (0–100%):

Risk = 100 × σ((24 − t50) / 4)

where σ is the logistic sigmoid function. When t50 is much shorter than 24 h, Risk approaches 100%; when t50 is much longer than 24 h, Risk approaches 0%.

The key relationships can also be written in MathML form:

m= qA3600 1000Lv , V= mρ , t50 = 0.5V V˙

How to Use the Calculator

  1. Tank volume (m³): Enter the liquid volume you expect to have in the tank. For small test tanks this might be 1–5 m³; large launch tanks can exceed 100 m³.
  2. Surface area (m²): Use the external surface area of the tank. Spherical tanks minimize area per unit volume; cylindrical tanks with domed ends have higher area. If you do not know the exact value, a first-order geometric estimate is sufficient.
  3. Heat leak rate (W/m²): This is the average heat flux through the insulation plus support penetrations. Typical orders of magnitude:
    • Well-insulated LH2 tanks with MLI: ~0.05–0.3 W/m²
    • Moderate insulation or aged systems: ~0.3–1 W/m²
    • Poorly insulated tanks or warm piping: >1 W/m²
  4. Latent heat of vaporization (kJ/kg): At typical storage conditions, LH2 is around 446 kJ/kg and LOX around 213 kJ/kg. Other cryogens (e.g., LNG, liquid methane, liquid nitrogen) have different values; use data consistent with your operating temperature and pressure.
  5. Liquid density (kg/m³): Representative densities near the normal boiling point are roughly 70 kg/m³ for LH2 and 1,140 kg/m³ for LOX. Density changes with temperature and subcooling; choose a value appropriate for your condition.

After entering the inputs, run the calculation to obtain:

Interpreting the Risk Score

The risk score is a compact indicator of how severe boil-off is relative to a one-day storage window. It is not a safety classification, but a planning aid. Use the following guidance as a rule of thumb:

Risk % Interpretation Operational guidance
0–25 Very slow boil-off Passive storage is usually acceptable for many hours to days. Good regime for long pre-launch holds or depot concepts.
26–60 Moderate loss rate Review insulation performance and minimize unnecessary dwell time. Consider topping off before launch or test.
61–100 Rapid loss High urgency to improve insulation, add active cooling, or shorten storage duration. Not suitable for long idle periods without additional control measures.

Worked Example

Consider a launch facility storing LH2 in a well-insulated spherical tank.

  1. Inputs:
    • Tank volume V = 10 m³
    • Surface area A = 50 m²
    • Heat leak rate q = 0.1 W/m²
    • Latent heat Lv = 446 kJ/kg
    • Density ρ = 70 kg/m³
  2. Total heat leak: Q̇ = q × A = 0.1 × 50 = 5 W.
  3. Energy absorbed per hour: Q = 5 × 3600 = 18,000 J.
  4. Mass boiled off per hour: Lv = 446 kJ/kg = 446,000 J/kg, so ṁ = 18,000 / 446,000 ≈ 0.040 kg/h.
  5. Volumetric boil-off rate: V̇ = 0.040 / 70 ≈ 5.7 × 10−4 m³/h.
  6. Time to 50% loss: Half the tank volume is 5 m³, so t50 = 5 / (5.7 × 10−4) ≈ 8,800 h (roughly 365 days).
  7. Risk score: Because t50 is much greater than 24 h, the logistic risk evaluates near 0%, indicating very slow boil-off relative to a one-day window.

In practice, this configuration would support long-duration storage with minimal mass loss, assuming the average heat leak assumptions are valid.

Comparison of Typical LH2 vs LOX Properties

While the calculator accepts arbitrary inputs, the table below highlights approximate property ranges for two common propellants at conditions near their normal boiling points. Use data from your specific design or test for detailed work.

Property Liquid hydrogen (LH2) Liquid oxygen (LOX)
Boiling temperature (approx.) 20 K 90 K
Latent heat of vaporization ~446 kJ/kg ~213 kJ/kg
Liquid density ~70 kg/m³ ~1,140 kg/m³
Typical well-insulated heat flux ~0.05–0.3 W/m² ~0.05–0.3 W/m²
Relative sensitivity to small heat leaks High (low density, high surface/volume) Moderate (higher density, often larger tanks)

Assumptions and Limitations

This calculator is intended as a first-order engineering and planning tool, not as a substitute for detailed cryogenic system design or safety review. Key assumptions include:

Because of these simplifications, results should be interpreted as indicative trends rather than certified performance predictions. For mission- or safety-critical decisions, use detailed thermal models, ground-test data, and formal engineering analysis in addition to this calculator.

Practical Use Cases and Next Steps

In launch operations, you can use the tool to check how long a cryogenic stage can sit on the pad before boil-off becomes operationally significant, to quantify the benefit of adding or improving insulation, or to compare different propellants for long-coast upper stages. Test facilities can use it for rough sizing of storage tanks and vent systems, and for estimating consumable losses over multi-shift campaigns.

For more refined studies, consider coupling these boil-off estimates with structural supports heat-leak models, line chilldown calculations, or detailed CFD/thermal simulations. Internal documentation or related tools on insulation performance and tank sizing can also complement the insights from this calculator.

Enter parameters to estimate boil-off.

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