Shulou(Shulou.com)11/24 Report--

CTOnews.com, November 1, this morning, after completing the relevant work, the long March 7 Jiayao 6 carrier rocket has been vertically transferred to position 201 of the Wenchang Space launch site of the Xichang Satellite launch Center, and plans to launch at the Wenchang Space launch site in the near future.

According to NOTAMS space data, the long March 7 Jiayao 6 carrier rocket is expected to launch from 22:00 to 23 p.m. on November 3. (CTOnews.com Note: the current load is unknown).

In addition, Hainan traffic police also issued a notice announcing the implementation of traffic control on the roads around the Wenchang space launch base and on the roads leading to Wenchang during the Wenchang rocket mission, and from 12:00 on November 3 to 12 on November 4.

According to public data, the first flight of the long March 7 was on June 25, 2016, while the first flight of the long March 7 to Yaoyi carrier rocket failed on March 16, 2020, and the follow-up telescopic rocket was successfully launched on March 12, 2021. The last launch was the remote 4 rocket launched on January 9, 2023 (Yao 5 was in 2022).

The long March 7 modified carrier rocket is a new generation of medium-sized high-orbit three-stage liquid fuel bundled carrier rocket developed by the Chinese Academy of launch vehicle Technology, which is mainly used for high-orbit satellite launch missions.

The long Seven A rocket is a medium-sized three-stage semi-cryogenic liquid carrier rocket developed by the first Institute of China Aerospace Science and Technology Corporation. It is composed of core one stage, core two stage, core three stage and four booster symmetrically tied around the core stage. The maximum length of the arrow is 60.13m, the diameter of the first and second stage of the core is 3.35m, the diameter of the third stage of the core is 3m, the diameter of the booster is 2.25m, the take-off mass is about 573t, the take-off thrust is 727t, its low-earth orbit (LEO) transport capacity is 17 tons (theoretical value), the geosynchronous transfer orbit (GTO) transport capacity is not less than 7 tons, and the earth-moon transfer orbit transport capacity (TLI) is 5 tons.

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