Experimental + reference-model benchmark

NASA K-Site LH₂ self-pressurization

A primary-source benchmark against NASA TM-105411. OffshoreLH2 is gated against NASA’s homogeneous reference because the present tank is a lumped equilibrium model; the measured stratified experiment is shown separately as model-form evidence.

PASS

What was tested

Quasi-steady pressure-rise rate and full pressure-versus-time response for a flightweight liquid-hydrogen tank under low wall heat flux.

Primary source

Van Dresar, N. T.; Lin, C. S.; Hasan, M. M. (1992), Self-Pressurization of a Flightweight Liquid Hydrogen Tank: Effects of Fill Level at Low Wall Heat Flux, NASA TM-105411 / AIAA-92-0818.

NASA NTRS record / paper

Values taken from NASA

QuantityValue usedNASA basis
Tank internal volume4.89 m³Experimental apparatus
Tank internal surface area14.0 m²Experimental apparatus
Initial pressure≈103 kPaTank reduced to atmospheric pressure before self-pressurization
Wall heat fluxes2.0 and 3.5 W/m²Figure 2 / test procedure
Cryoshroud temperatures294 K and 350 KUsed to obtain the two nominal heat fluxes
Fill levels29%, 49%, 83–83.5%Figure 2 and earlier 83% campaign
Experimental sampling0.5 hPaper states data were sampled at 1/2-hour intervals
Starting conditionSteady boil-offFigure 2 dataset

Quasi-steady pressure-rise results

The acceptance rule was fixed at ≤10% relative error against NASA’s published homogeneous-theory slope.

q″FillNASA measuredNASA homogeneousOffshoreLH2Error vs homogeneousStatus
2.0 W/m²29%3.820 kPa/h2.7302.47169.465%PASS
3.5 W/m²29%8.2104.8304.93822.240%PASS
2.0 W/m²49%2.7201.8601.97196.017%PASS
3.5 W/m²49%6.0703.7103.80132.460%PASS
0.35 W/m²83.5%0.2230.1980.205253.661%PASS
2.0 W/m²83.5%3.4701.4601.36246.688%PASS
3.5 W/m²83.5%8.1402.6302.72043.436%PASS

Full pressure-time results

Figure 2 was digitized from the primary NASA PDF. The predeclared gate is pressure-rise NRMSE ≤10% against the NASA homogeneous curve.

CasePressure-rise NRMSEStatus
2.0 W/m², 29%2.30%PASS
2.0 W/m², 49%3.36%PASS
2.0 W/m², 83%4.58%PASS
3.5 W/m², 29%0.32%PASS
3.5 W/m², 49%0.98%PASS
3.5 W/m², 83%1.73%PASS

Measured stratified experiment

The measured NASA pressure rise is higher than the homogeneous prediction because the real tank develops gravity-driven thermal stratification and natural convection. OffshoreLH2 does not resolve those spatial effects, so this comparison is deliberately descriptive only. The disagreement is retained rather than tuned away.

Digitization check: fitted slopes from the digitized experimental markers reproduce NASA Table 1 within 0.31–2.41% across the six pressure-time cases.

Reproducibility

  • reference/nasa_k_site_pressure_timeseries_digitized.csv
  • reference/nasa_k_site_pressure_timeseries_PROVENANCE.md
  • validation_cases/lh2_nasa_k_site/timeseries.cpp
  • scripts/analyze_nasa_k_site_timeseries.py