Laboratory Cabin Module

Laboratory Cabin Module

A model of Tiangong-2, the prototype for the LCMs
Module statistics
Launch date	24 July 2022: Wentian 31 October 2022: Mengtian
Launch vehicle	Long March 5B
Mass	~21,500 kg (47,400 lb) (dry mass of each LCM)
Length	17.9 m (59 ft)
Diameter	4.2 m (14 ft)

The Laboratory Cabin Modules (LCM) (Chinese: 实验舱) are components of the Tiangong space station. Based on the Tiangong-2 experimental space module, the LCMs complete the third and final stage of Project 921, the CNSA's program to establish a permanent Chinese space station. While China's small uncrewed spacecraft can provide platforms for zero gravity and exposure to space for scientific research, the LCMs offer a long term environment combined with ready access by human researchers over periods that far exceed the capabilities of Shenzhou spacecraft. Operations are controlled from the Beijing Aerospace Command and Control Center in China.

The first LCM, Wentian (simplified Chinese: 问天; traditional Chinese: 問天; pinyin: Wèn Tiān; lit. 'Quest for the Heavens^[1]'), was launched into orbit on 24 July 2022. The second LCM, Mengtian (simplified Chinese: 梦天; traditional Chinese: 夢天; pinyin: Mèng Tiān; lit. 'Dreaming of the Heavens^[1]'), was launched into orbit on 31 October 2022.^[2]

The first laboratory module provides additional navigation avionics, propulsion and orientation control as backup functions for the Tianhe core module (TCM). Both LCMs provide a pressurized environment for researchers to conduct science experiments in freefall or zero gravity which could not be conducted on Earth for more than a few minutes. Experiments can also be placed on the outside of the modules, for exposure to the space environment, cosmic rays, vacuum, and solar winds.

The axial ports of the LCMs are fitted with rendezvous equipment, and each first docked to the axial port of the CCM. A mechanical arm dubbed the Indexing Robotic Arm, somewhat like the Lyappa arm used on the Mir space station, moved Wentian to a starboard-side port and Mengtian to a port-side port of the CCM.^[3] It is different from Lyappa as it works on a different mechanism. Lyappa arm is needed to control the pitch of the spacecraft and redocking in a different plane. But the Indexing Robotic Arm is used when docking is needed in the same plane. In addition to this arm used for docking relocation, the Chinarm on Tianhe module can also be used as a backup in place of Indexing Robotic Arm.^[4][5]

Wentian was successfully relocated to the starboard port on 30 September 2022 at 04:44 UTC^[6] using the indexing robot arm.

In addition to this, Wentian houses a small 5 m (16 ft) long robotic arm like the Chinarm as a supplemental to that arm. It is used for manipulating extravehicular payloads and their positioning accuracy is 5 times better than the Chinarm. There are standard adapters (silver squares) on the modules to host the payloads.^[7] There is also an adapter by which one of these arms can be grappled by the Chinarm it to work a single robotic arm like Orbiter Servicing Arm with Canadarms.^[8]

Mengtian also carries a toolbox equipped with a dexterous robotic arm (similar to the Lyappa arm used on the Mir space station) installed to assist in cargo transfer and payload release, and can be used to deploy external payloads.^[9][10]

Electrical power is provided by two steerable solar power arrays, which use photovoltaic cells to convert sunlight into electricity. Energy is stored to power the station when it passes into the Earth's shadow. Resupply ships will replenish fuel for LCM 1 for station-keeping, to counter the effects of atmospheric drag.

The length of each module is 17.9 m. They are cylindrical with a maximum diameter of 4.2 m and an on-orbit mass of approximately 20,000 kg (44,000 lb) apiece.^[11][12]

Both modules were launched in 2022 on Long March 5B launch vehicles from Wenchang Satellite Launch Center. Wentian was launched on 24 July 2022, while Mengtian was launched on 31 October 2022.^[2] They were inserted into a low Earth orbit with an average altitude of 393 km (244 mi) at an orbital inclination of 42 degrees, centered in the Earth's thermosphere.^[11][13]

• Tianhe core module

• Chinese Space Agency website