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Long March 8A

China Aerospace Science and Technology Corporation · Cina

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.

Costruttore
China Aerospace Science and Technology Corporation
Primo volo
11 febbraio 2025
Lanci
11
Riusciti
11
Falliti
0
Tasso di successo
100%
In programma
1
Altezza
50,5 m
Diametro
3,35 m
Massa al decollo
371 t
Carico in orbita bassa
9.800 kg
Carico in orbita di trasferimento geostazionaria
3.500 kg
Riutilizzabile
no

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