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Clean Hydrogen Partnership

Damage to the insulation sell of a LH2 tank

Event

Event ID
459
Quality
Description

During the warm-up phase of a large liquid hydrogen sphere, the annular space was over-pressurised and perlite insulation was expelled through the evacuation nozzle and the burst diaphragm. Air had leaked into the annular space some weeks earlier and repairs had been carried out. However, the air had solidified in the annular space. During the warm-up, the air vaporised and caused a pressure build-up. The vessel sustained minor damage.

Event Initiating system
Classification of the physical effects
No Hydrogen Release
Nature of the consequences
Macro-region
North America
Country
United States
Date
-
Component involved
cryogenic insulation shell
Failure mode
internal explosion
Initiating cause
over-pressurisation
Root CAUSE analysis

Leak points had been found in the external shell and sealed approximately six weeks prior to this event. The event was due to a lack of design considerations for monitoring/ evaluating the tank conditions during warmup. The hazards involved in making temporary repairs in the evacuation system were not identified.
Therefore, the ROOT CAUSES were shortcoming in repairing procedures and in evaluating the related risks.

Root causes
Date entry in HIAD
01/11/2025

Facility

Application
Non-road vehicles
Sub-application
Aerospace
Hydrogen supply chain stage
All components affected

LH2 vessel

Process temperature range [C]
cryogenic temperature (below -50°C)
Location type
Open
Location
industrial area
Operational condition
Pre-event occurrences

leaks in the external shell of the vessel had been repaired six week before.

Emergency & Consequences

Number of fatalities
0
Number of injured persons
0
Post-event summary

Minor damage to the vessel

Lesson Learnt

Lesson Learnt

This is a rare case of deterioration of the annular space serving the insulation of a LH2 vessel, due to overpressure. It happened during the warming up of the vessel (which was highly probably almost empty), a procedure starting with the reduction of the vacuum in the insulation shell.
A possible escalation could have been the over-pressurisation of the internal shell due to too rapid heat inlet. Nevertheless, since the final goal of the operation as to bringing the vessel to room temperature, it is expected that venting system would have been able to deal with a higher hydrogen flow than the one planned. The vessel was anyhow equipped with pressure relief devises in case of internal over-pressurisation.

In-depth data

Release type
gas
Involved substances (% vol)
H2 100%
Probable IGNITION SOURCE
Explosion type

References

Sources categories
ORDIN
Reference & weblink

Mishap no 86 in
P. L. Ordin, Review of hydrogen accidents and incidents in NASA operations, 1974, NASA TM X-71565
https://ntrs.nasa.gov/citations/19740020344

Hankinson and Lowesmith, Qualitative Risk Assessment of Hydrogen Liquefaction, Storage and Transportation, FCH JU project IDEALHY, Deliverable 3.10 (2013)
confidential
(accessed October 2025)

Lowesmith et al., Safety issues of the liquefaction, storage and transportation of liquid hydrogen: An analysis of incidents and HAZIDS, Int. J. Hydrogen energy (2014) https://doi.org/10.1016/j.ijhydene.2014.08.002