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Long March 8A

Long March 8A

Long March family · built by China Aerospace Science and Technology Corporation · maiden flight 2025-02-11

Profile data last updated: 2026-08-15T20:08:04.839063+00:00 | 7531-09-01

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.

Specifications

50.5 mLength
3.35 mDiameter
371 tLaunch mass
2Stages
4800 kNLiftoff thrust

Payload Capacity

9800 kgTo LEO
3500 kgTo GTO

Lifetime Launch Record

As reported by Launch Library 2 across this rocket's entire history, not just the launches tracked on this site.

10Total launches
10Successful
0Failed
0Upcoming

Launches Tracked on This Site

10In our archive
100.0%Success rate
Feb 11, 2025 09:30 UTCEarliest tracked
Aug 04, 2026 08:52 UTCMost recent
MissionDateStatus
Long March 8A | SatNet LEO Group 23 Aug 04, 2026 08:52 UTC Success
Long March 8A | SpaceSail Polar Group #14 Jul 05, 2026 13:43 UTC Success
Long March 8A | SatNet LEO Group 20 Mar 12, 2026 19:48 UTC Success
Long March 8A | SatNet LEO Group 18 Jan 13, 2026 15:25 UTC Success
Long March 8A | SatNet LEO Group 17 Dec 25, 2025 23:26 UTC Success
Long March 8A | SatNet LEO Group 14 Dec 06, 2025 07:53 UTC Success
Long March 8A | SatNet LEO Group 12 Oct 16, 2025 01:33 UTC Success
Long March 8A | SatNet LEO Group 10 Aug 25, 2025 19:08 UTC Success
Long March 8A | SatNet LEO Group 06 Jul 30, 2025 07:49 UTC Success
Long March 8A | SatNet LEO Group 02 (Demo Flight) Feb 11, 2025 09:30 UTC Success

Wikipedia