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Launch Vehicles
Vehicle family profile

Long March 10

Family-level launch record combining canonical variants, historical missions, public cadence forecasts, and available payload performance specs.

Manufacturer unknownUnknown
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Variants
0
Canonical variants linked to this family.
Historical missions
0
Missions in the public mission table with actual launch dates.
Peak listed capacity
Unknown
Maximum payload capacity across listed variants and orbits.

Launch Cadence

Historical missions are grouped by actual launch year. Forecast cadence uses family-level launch-rate rows.

YearHistorical missionsForecast launches

No cadence data

No historical mission years or launch-rate forecast rows are linked to this family.

Performance Specs

Payload capacity by variant and target orbit when structured capacity rows are available.

VariantOrbitCapacityAltitudeInclinationSource

No performance specs

No structured payload capacity rows are linked to this vehicle family.

Recent Missions

Latest launched missions using variants in this family.

MissionVariantLaunch

No recent missions

No launched missions are linked to variants in this family.

Forecasted Missions

Upcoming mission rows with announced launch timing.

MissionVariantAnnounced

No forecasted missions

No upcoming announced mission rows are linked to this vehicle family.

Variants

Canonical variants rolled up into this launch vehicle family.

VariantStagesMissionsStatus

No variants

No canonical variants are linked to this vehicle family.

Entity Mentions
All verified mentions of this entity in source documents

Engineers consider the Long March 10 rocket and the Mengzhou spacecraft core elements of China’s roadmap to land astronauts on the moon before the end of the decade.

Mentioned as: Long March 10Source

Engineers state that the first two stages of the Long March 10 core booster are essentially common to both the lunar and the shorter space-station variants.

Mentioned as: Long March 10Source

The Long March 10 lunar-mission configuration can send at least 27 tons of payload onto an Earth-moon transfer trajectory.

Mentioned as: Long March 10Source

The maritime recovery followed a flight test of the Long March 10 first-stage booster integrated with the Mengzhou crewed spacecraft.

Mentioned as: Long March 10Source

The Long March 10 first-stage booster performed a controlled return using its engines and grid fins before a splashdown in a preselected area of the South China Sea.

Mentioned as: Long March 10Source

The shorter Long March 10 variant will be capable of carrying 14 tons to low Earth orbit.

Mentioned as: Long March 10Source

A shorter variant of the Long March 10 without side boosters is under development and will be 67 meters tall with a liftoff mass of about 740 tons.

Mentioned as: Long March 10Source

A crane lifted the recovered Long March 10 booster from the water and placed it on a recovery vessel for transport and subsequent analysis.

Mentioned as: Long March 10Source

The standard lunar-mission configuration of Long March 10 consists of a central core booster flanked by multiple side boosters.

Mentioned as: Long March 10Source

The shorter Long March 10 configuration for Tiangong resupply flights will omit the third stage to optimize the vehicle for low Earth orbit operations.

Mentioned as: Long March 10Source

The Long March 10A test booster continued its flight after the Mengzhou capsule test, performed a simulated catch next to the autonomous recovery ship Linghangzhe and splashed down in the South China Sea.

Mentioned as: Long March 10ASourceFeb 15, 2026

An extension was placed atop the Long March 10 series static fire article to install four grid fins and catch hooks, creating the Long March 10A test booster.

Mentioned as: Long March 10SourceFeb 15, 2026

An extension was placed atop the Long March 10 series static fire article to install four grid fins and catch hooks, creating the Long March 10A test booster.

Mentioned as: Long March 10ASourceFeb 15, 2026

The Long March 10A test booster passed just above the Kármán line and reached a peak altitude of 105 kilometers during its February 11 flight.

Mentioned as: Long March 10ASourceFeb 15, 2026

Recovery teams retrieved the Long March 10A test booster’s remaining lower half and concluded recovery operations on February 13, 2026.

Mentioned as: Long March 10ASourceFeb 15, 2026

The Long March 10 rocket’s third stage uses three hydrogen-burning YF-75DA engines.

Mentioned as: Long March 10SourceFeb 15, 2026

The Long March 10A test booster performed a pseudo-entry burn during its flight to demonstrate part of reusable first-stage flight.

Mentioned as: Long March 10ASourceFeb 15, 2026

The Long March 10A test booster guided itself next to the recovery ship Linghangzhe and performed a planned hover five meters above the sea.

Mentioned as: Long March 10ASourceFeb 15, 2026

Two grid fins were deployed on the Long March 10A test booster during reentry, and one grid fin failed to unfurl correctly, leading flight computers to command the fin opposite to remain stowed.

Mentioned as: Long March 10ASourceFeb 15, 2026

The Long March 10A test booster’s boilerplate upper half sheared off upon contact with the sea surface after splashdown.

Mentioned as: Long March 10ASourceFeb 15, 2026
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