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Space · launch vehicle

Long March 8A

CASC ACTIVE
At a glance
Launches
11
Success rate
100%
11 ok · 0 failed
Payload to LEO
9,800 kg
Payload to GTO
3,500 kg
Status
Active
First flight
11 Feb 2025
Reusable
No
Height
50.5 m
Diameter
3.35 m
Launch mass
371 t
Liftoff thrust
4,800 kN
Stages
2
Launch cost
—
Booster landings
—
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Next flight
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About

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.