| H 2 | |
|---|---|
| Launch vehicle | H 2 |
| Launch site | Tanegashima Space Centre, Tanegashima, Japan |
| Date/Time | 1998-02-21 |
| Description | Second stage partial failure |
| Cause | Cumbustion chamber leak |
| Payload | Comets [Takehashi] (Experimental satellite, NASDA, Japan) |
| Desired orbit | Geostationary transfer orbit |
|
About seven seconds before the engine stopped, a series of malfunctions had occurred, including damage to the electricity system and the overheating of various engine parts. NASDA suspects that there was a leak of at least 5 cm2 that let some of the hot fuel gas escape from the combustion chamber. The gas damaged the system of pipes and electricity wires and eventually stopped the engine. |
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