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At  7th July , 2026 Beijing time, the Long March 10B Yao 1 carrier rocket began erection at Launch Complex 2 of the CNSA – China National Space Administration-  Hainan Commercial Space Launch Center, Hainan Province, China, People’s Republic of China. . At midnight on July 7, the Long March 10B Y1 carrier rocket was successfully transferred to Launch Pad 2 at the Hainan Commercial Space Launch Site.

China Achieves First Controlled Rocket Recovery -Long March 10B Rocket Successfully Achieves Controlled Recovery of First Stage

At 12:15 PM on July 10, 2026, the Long March 10B carrier rocket launched from the Hainan Commercial Space Launch Site. Approximately six minutes after the first and second stages separated, the first stage returned vertically and was successfully recovered on a sea-based recovery platform.


This marks China’s first successful controlled recovery of a carrier rocket’s first stage, and also the world’s first network-based recovery of a carrier rocket. [Long March 10B Rocket Successfully Achieves Controlled Recovery of First Stage] At 12:15 PM on July 10, 2026, the Long March 10B carrier rocket launched from the Hainan Commercial Space Launch Site. Approximately six minutes after the first and second stages separated, the first stage returned vertically and was successfully recovered on a sea-based recovery platform.

This marks China’s first successful controlled recovery of a carrier rocket’s first stage, and also the world’s first network-based recovery of a carrier rocket.

At 12:15 on July 10, 2026, the Long March 10B carrier rocket successfully completed the world’s first net-system recovery of a carrier rocket at the Hainan Commercial Space Launch Site. The first stage landed vertically and was precisely captured by the sea platform.

 

 

I. Task Overview

II. Highlights of Grid-Based Recycling Technology

III. Rocket Core Parameters

Parametersindex
configurationThe arrow has a two-stage, smooth shaft design, a body diameter of 5 meters, and a total height of nearly 70 meters.
Core Level 1 PowerSeven YF-100N liquid oxygen/kerosene engines (reusable), with a takeoff thrust of approximately 892 tons.
Secondary powerYF-219 Liquid Oxygen Methane Engine
Recovery status capacityLow Earth orbit ≥16 tons, 900 km SSO orbit ≥11 tons
Reuse TargetThe first stage has been reused more than 10 times, and the rocket body has a turnover time of approximately 72 hours.

IV. Recycling Process

Images and visuals are from their Respectives CMS China Manned SpaceCNSA-China National Space Administration

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