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Clean Hydrogen Partnership

Fire in the test chamber of a rocket LH2 tank

Event

Event ID
399
Quality
Description
During preparation of a spacecraft LH2 tank in an environmental test chamber, a liquid hydrogen fire occurred in the chamber. The tank was being "topped off" at the time. Damage was caused to the facility and test system.

[Ordin, NASA (1974)]
Event Initiating system
Classification of the physical effects
Hydrogen Release and Ignition
Nature of the consequences
Fire (No additional details provided)
Macro-region
North America
Country
United States
Date
-
Main component involved?
Reactor / Oven / Furnace / Test Chamber
How was it involved?
Internal Explosion (H2-Air Mixture)
Root causes
Root CAUSE analysis
Air had entered the system through the vent line quick disconnects. Ignition occurred as a result of bare wires in the heater access hole. A protective insulation grommet had inadvertently been omitted. The discrepancy had not been identified by inspection. ROOT CAUSES are related to an error in the execution of one preparatory step and in failing to identify it during inspection. Moreover, vent are expected to be designed to avoid or limit as far as possible entrance of air, preventing formation of explosive gas mixture.

Facility

Application
Non-Road Vehicles
Sub-application
Aerospace
Hydrogen supply chain stage
All components affected
environnmental test chamber
Location type
Unknown
Operational condition
Description of the facility/unit/process/substances
ENVIROMENTAL TESTING CHAMBER FOR THE ARTEMIS
NASA used different environmental chambers for cryogenic and structural testing for the Saturn V liquid hydrogen stage, loacated atdifferent R&D centres . The source reporting this event does not clarify the type of tests performed. It cn be guessed that it was a cryogenic proof tests, Fior example, the 3rd March 1968, a Saturn V second stage (S-II-4) underwent its first cryogenic proof test at the Mississippi Test Facility, now NASA's Stennis Space Centre).

WHAT IS A GROMMET?
An insulation grommet is a small, ring-shaped component, usually made of rubber, that is inserted into a hole to protect wires, cables, or hoses passing through it from sharp edges and abrasion. They are also used for electrical insulation, shock absorption, and creating a seal against dust, moisture, and vibration.

Emergency & Consequences

Number of injured persons
0
Number of fatalities
0
Environmental damage
0
Post-event summary
test facility and test system damaged

Lesson Learnt

Lesson Learnt
On the recurrence of air into vent stacks during NASA programme, see for example Rhodes, R., Explosive lessons in hydrogen safety, Ask Magazine 2013 (https://appel.nasa.gov/wp-content/uploads/2013/04/513855main_ASK_41s_explosive.pdf).

Event Nature

Release type
liquid
Involved substances (% vol)
H2 100%
Release duration
unknown
Presumed ignition source
Electricity
Ignition delay
N

References

Reference & weblink

Mishap no 59 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/19740020344

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

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