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.
[Ordin, NASA (1974)] - Event Initiating system
- Classification of the physical effects
- No Hydrogen Release
- Nature of the consequences
- Macro-region
- North America
- Country
- United States
- Date
- -
- Main component involved?
- Cryogenic Insulation Shell
- How was it involved?
- Internal Explosion (Hp Explosion)
- Initiating cause
- Over-Pressurisation (Loss Of Vacuum)
- Root causes
- 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 reĀpairs in the evacuation system were not idenĀtified.
Therefore, the ROOT CAUSES were shortcoming in repairing procedures and n asesing the related risks.
Facility
- Application
- Hydrogen Stationary Storage
- Sub-application
- aerospace
- Hydrogen supply chain stage
- Hydrogen Storage (No additional details provided)
- All components affected
- LH2 vessel
- Location type
- Open
- Location description
- 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 injured persons
- 0
- Number of fatalities
- 0
- Environmental damage
- 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.
Event Nature
- Release type
- gas
- Involved substances (% vol)
- H2 100%
- Release duration
- unknown
- Presumed ignition source
- No release
References
- Reference & weblink
Mishap no 86 in <br />
P. L. Ordin, Review of hydrogen accidents and incidents in NASA operations, 1974, NASA TM X-71565<br />
https://ntrs.nasa.gov/citations/19740020344Lowesmith 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
Hankinson and Lowesmith, Qualitative Risk Assessment of Hydrogen Liquefaction, Storage and Transportation, FCH JU project IDEALHY, Deliverable 3.10 (2013)<br />
confidential<br />
(accessed October 2025)
JRC assessment
- Sources categories
- ORDIN