H3-30 · Test Flight

Test flight of the H3-30 variant of the H3 launch vehicle with 3 LE-9 engines in the first stage and no SRBs. The flight will carry a dummy main payload (Vehicle Evaluation Payload 5, VEP-5) and several hitchhiking small satellites: * PETREL * STARS-X * BRO-22 * VERTECS * HORN-L/R
First upwards movement of the rocket
Separation of the payload fairing
Cut-off of the main engine
Separation of the second stage from the first
First start of the second engine
First cut-off of the second engine
Start of the payload deployment sequence
End of the payload deployment sequence.
Second start of the second engine
Second cut-off of the second engine
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No changes recorded
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The H3 Launch Vehicle is an expendable launch system in development in Japan. H3 rockets are liquid-propellant rockets with strap-on solid rocket boosters and are planned to be launched from the Tanegashima Space Center in Japan. Mitsubishi and the JAXA have been responsible for the design, manufacture, and operation of the H3.
H3-30 Test Flight
Payload details are described in the mission overview. No independently structured payload manifest or payload mass has been provided by the source.
Yoshinobu Launch Complex LP-2
Tanegashima Space Center, Japan
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