Tianhe

Launch Success

Liftoff Time (GMT)

03:23:15

Thursday April 29, 2021

Watch Replay

Official Livestream

Mission Details

Read Article

Launch Notes

First module of the new Chinese space station. Third Chinese space station, and the first modular space station to be launched this century.

Tianhe

Wiki

Tianhe is the first module of the new Chinese space station. The Central Module controls the orbit of the Station, mirroring the role played by the Russian Zvezda module of the International Space Station, and serves as a place to live and work. It has integrated racks containing scientific experiments and five docking ports. Its architecture is very similar to that of the Zvezda module: it consists of two cylinders of different diameters placed end to end with a spherical module in the extension of the cylinder of smaller diameter serving as an airlock with 4 docking ports. The androgynous docking system is identical to the one used by the existing Chinese vessels: it is a Russian version of the APAS-89 implemented on board the Buran shuttle, Mir, and the Russian module of the International Space Station. The spherical part includes in its upper part a hatch for extra-vehicular exits while the docking port located in the lower part seems to be reserved for Shenzhou vessels. Tianhe is 14.1 meters long with a diameter of 4.2 meters. Its mass is about 22 tons. The module has a large robotic arm attached to the smaller diameter cylinder. It also has two large deployable solar panels, each measuring 11 by 4.6 meters.

Low Earth Orbit

1 Payload

22,500 kilograms

Rocket

Active
Long March 5B

Active Since 2020

China Aerospace Science and Technology Corporation logo

Agency

CASC

Rocket

Height: 53.66m

Payload to Orbit

LEO: 23,000 kg

GTO: 0 kg

Liftoff Thrust

10,565 Kilonewtons

Fairing

Diameter: 5.2m

Height: 20.5m

Stages

2

Strap-ons

4

Launch Site

LC-101

Wenchang Space Launch Site, China

Fastest Turnaround

69 days 21 hours

Stats

Long March 5B


2nd

Mission

1st

Mission of 2021

2021


36th

Orbital launch attempt