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Long March 8A

China Aerospace Science and Technology Corporation · China

The Long March 8A is an orbital launch vehicle developed by the China Academy of Launch Vehicle Technology based on the Long March 8. It has an increased capability of up to 7 tonnes to a 700 km altitude sun-synchronous orbit. It implements a larger 3.35 meters diameter liquid hydrogen/liquid oxygen 2nd stage, coupled with 2 upgraded version of the YF-75D engines used on the Long March 5 (known as the YF-75H) with increased thrust to 10 tonnes each through measures such as increased turbopump speeds. The Long March 8A can also use a larger 5.2 meters diameter payload fairing.

Hersteller
China Aerospace Science and Technology Corporation
Erstflug
11. Februar 2025
Starts
11
Erfolgreich
11
Fehlgeschlagen
0
Erfolgsquote
100%
Geplant
1
Höhe
50,5 m
Durchmesser
3,35 m
Startmasse
371 t
Nutzlast in den niedrigen Erdorbit
9.800 kg
Nutzlast in den geostationären Transferorbit
3.500 kg
Wiederverwendbar
nein

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