
10th Anniversary of the Maiden Flight of the New Generation Medium-lift Rocket Long March 7!
At 20:00 on June 25, 2016, the Long March-7 Y1 carrier rocket/Yuanzheng-1A upper stage was launched from Launch Complex 2 at the Wenchang Space Launch Site in China, People’s Republic of China , subsequently sending multiple payloads, including a scaled-down return capsule of a multi-purpose spacecraft, into low Earth orbit. This mission marked the first launch from the Wenchang Launch Site and the maiden flight of the Long March-7 carrier rocket. The Long March-7 will celebrate its 10th anniversary of its maiden flight on June 25, 2026.
Early members of the Long March 5 series

The Long March 7 is a medium-sized version of the Long March 5 series of carrier rockets, which was originally planned as part of China’s new generation of Long March carrier rockets. Its booster stage, core stage, and core stage use the original Long March 5 series’ 2.25-meter diameter liquid oxygen/kerosene module, 3.35-meter diameter liquid oxygen/kerosene module, and 3.35-meter diameter core stage liquid oxygen/kerosene module, respectively, corresponding to the original Long March 5 series’ medium-sized two-and-a-half-stage carrier rocket.
Due to planning adjustments, the Long March 7 and Long March 6 were separated from the initial Long March 5 series rockets, forming separate medium and small models, and embarking on an independent development path.



Former manned rockets
The Long March 7 rocket was initially designed as a kerosene-fueled version of the Long March 2F (CZ-2F/H), retaining the same diameter rocket body for each stage, but replacing all main engines with liquid oxygen-kerosene engines. It was originally planned for launches of the Shenzhou manned spacecraft and the Tianzhou cargo spacecraft, but was later repurposed for cargo spacecraft launches.
The Long March 7 adopts a two-and-a-half-stage configuration. The booster stage uses four 2.25-meter diameter boosters, each equipped with one single-pendulum YF-100 liquid oxygen-kerosene engine; the core stage has a diameter of 3.35 meters and is equipped with two double-pendulum YF-100 engines; the core stage has a diameter of 3.35 meters and is equipped with four YF-115 engines (two double-pendulum and two non-pendulum); the fairing is the same 4.2-meter diameter fairing as the Long March 2FT.

The Long March 7 rocket is 53.075 meters tall, has a takeoff mass of about 597 tons, a takeoff thrust of 727 tons, a low Earth orbit (LEO) payload capacity of about 14 tons, a payload factor of about 2.35%, and a 700-kilometer circular sun-synchronous orbit (SSO) payload capacity of 5.5 tons.
Built to manned rocket standards, the Long March 7 boasts a reliability index of 0.98, necessitating a highly redundant design with multiple backups for critical equipment such as the flight control computer. These features significantly increase the rocket’s weight. Furthermore, to adapt to the windy and rainy conditions at the Wenchang launch site, the Long March 7 incorporates specific design features. The entire rocket is waterproof, enabling launches in moderate rain; its wind resistance has been enhanced, allowing for transport in winds up to force 8 and launches in winds expected only once every ten years. These additional design features to adapt to weather conditions have also contributed to the rocket’s overall weight.
The Long March 7 rocket achieved a reliability of 0.9871, contributing to the successful completion of 11 launches over 10 years. However, its high redundancy and wind/water resistant design resulted in a relatively large rocket weight, leading to a lower payload coefficient. Among the new generation of Long March launch vehicles, the Long March 7’s near-Earth payload coefficient of 2.35% is considered low.


The basic model of the new generation Long March rocket
The Long March 7 is the first medium-lift rocket and maiden flight model of the new generation of Long March carrier rockets. It was developed using the design concept of “modularization, combination and serialization” and different mission models were derived according to mission requirements.
The Long March 7A is a high-orbit rocket. Based on the Long March 7, it features a 3-meter diameter hydrogen-oxygen final stage (core stage) and undergoes adaptive modifications. This rocket corresponds to the original Long March 5 series, a medium-lift high-orbit launch vehicle with a three-and-a-half-stage configuration and a hydrogen-oxygen final stage. It is primarily used for medium-to-high Earth orbit launch missions and is planned to replace the previous generation of high-orbit dedicated launch vehicle, the Long March 3B.

The Long March 8 series is a dedicated launch vehicle for low-Earth orbit (LEO) constellations. Based on the Long March 7’s launch stage, the pair of diagonally opposite boosters are removed, and a 3-meter diameter hydrogen-oxygen final stage is added, forming the basic Long March 8 configuration with two boosters and two and a half stages. Removing the two boosters from the basic Long March 8 configuration results in the Long March 8 single-core stage configuration. Replacing the final stage with a 3.35-meter diameter hydrogen-oxygen final stage (core two-stage) on the basic Long March 8 configuration creates the Long March 8A. The Long March 8 series is primarily used for launch missions such as LEO constellation networking.
In the new generation of Long March rockets, the Long March 7 is the technological foundation for the development of the Long March 7 and Long March 8 series, supporting the development of five rocket models in the two series. It is a true basic model of the new generation of Long March rockets.

The Long March 10A will take over from the Long March 7 in launching the Tianzhou spacecraft.
Currently, the Long March 7 rocket is mainly used for launching the Tianzhou cargo spacecraft, serving as the dedicated cargo train for the Tiangong space station. As the Tiangong space station enters a phase of routine operation, cost reduction and efficiency improvement have become more prominent. As a expendable launch vehicle, the Long March 7, while highly reliable and accurate in orbital insertion, is not cost-effective. To reduce cargo launch costs, alternative solutions are needed, and using reusable rockets is one of the best options.
The Long March 10 series includes two manned spaceflight models with four configurations. The Long March 10A cargo configuration is used to launch the Tianzhou cargo spacecraft. The Long March 10A cargo configuration employs a two-stage tandem configuration, with the first stage supporting multiple recoveries and reuses. This rocket is 66.4 meters high, 5 meters in diameter, and has a launch mass of approximately 750 tons. In its single-use state, its low Earth orbit (LEO) payload capacity is around 20 tons; with the first stage recovered, its LEO payload capacity is no less than 14.2 tons. In its recovered state, the Long March 10A cargo version can meet the full-load launch requirements of the Tianzhou spacecraft, and its launch cost is lower, making it a potential replacement for the Long March 7. The Long March 7, however, will need to find alternative deployment methods.
Conclusion
The Long March 7, initially designed for manned launches and later used for cargo launches, will be replaced by the Long March 10A cargo version, its role constantly evolving. As the basic model of the new generation of Long March rockets, by sharing the core stage and boosters, and with the increasing launch frequency of the Long March 7A and Long March 8 series, the launch cost of the Long March 7 rocket will be further reduced. When the Long March 7 retires from manned space missions, through simplified configuration and weight reduction, its carrying capacity and efficiency can be significantly improved, while reducing the launch cost per unit mass, making it a launch vehicle with greater carrying capacity, lower cost, and sufficient reliability.
Designed for low Earth orbit (LEO) missions, the Long March 7 offers significant sun-synchronous orbit and low Earth orbit (LEO) payload capacity, supporting the mass deployment of LEO constellations and the launch of large LEO remote sensing satellites. This will effectively cover the launch needs of military, civilian, and commercial satellites in the LEO range. Therefore, even if its role changes in the coming years, the Long March 7 will remain one of China’s main launch vehicle models, providing high-quality launch services at a reasonable cost.
Images and visuals are from their Respectives CMS China Manned SpaceCNSA-China National Space Administration



























