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/19740020344Hankinson 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