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Long March · China Aerospace Science and Technology Corporation

Long March 8A

active
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Specifications

Status
active
Height
50.5 m
Diameter
3.35 m
Mass
371,000 kg
Stages
2
Payload to LEO
9,800 kg
Payload to GTO
3,500 kg
First flight
2025-02-11
Total launches
8
Success / Fail
8 / 0

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.

Payloads it launched · 72

HULIANWANG DIGUI-155
LEO
HULIANWANG DIGUI-158
LEO
HULIANWANG DIGUI-159
LEO
HULIANWANG DIGUI-156
LEO
HULIANWANG DIGUI-157
LEO
HULIANWANG DIGUI-160
LEO
HULIANWANG DIGUI-162
LEO
HULIANWANG DIGUI-163
LEO
HULIANWANG DIGUI-161
LEO
HULIANWANG DIGUI-139
LEO
HULIANWANG DIGUI-145
LEO
HULIANWANG DIGUI-138
LEO
HULIANWANG DIGUI-142
LEO
HULIANWANG DIGUI-143
LEO
HULIANWANG DIGUI-137
LEO
HULIANWANG DIGUI-140
LEO
HULIANWANG DIGUI-141
LEO
HULIANWANG DIGUI-144
LEO
HULIANWANG DIGUI-128
LEO
HULIANWANG DIGUI-133
LEO
HULIANWANG DIGUI-134
LEO
HULIANWANG DIGUI-130
LEO
HULIANWANG DIGUI-131
LEO
HULIANWANG DIGUI-129
LEO