Laboratory Cabin Module

From Wikipedia, the free encyclopedia
Jump to navigation Jump to search

Laboratory Cabin Module
CZ-5 launch vehicle model.JPG
A model of the LCM launcher, the Long March 5
Module statistics
Launch date 2021: Wentian
2022: Mengtian[1]
Launch vehicle Long March 5
Mass 20-22 thousand kg
Length 14.4m
Diameter 4.2m

The Laboratory Cabin Modules (LCM)s are a major element of the Chinese space station, based on Tiangong-2, as the final stage of Project 921 Tiangong, part of the Chinese space program. While China's small unmanned 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 will be controlled from the Beijing Aerospace Command and Control Center in the People's Republic of China.

Purpose

The first laboratory module will provide additional navigation avionics, propulsion and orientation control as backup functions for the Core Cabin Module (CCM). 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 port of the LCMs will be fitted with rendezvous equipment and will first dock to the axial port of the CCM. A mechanical arm similar to the Russian Lyappa arm used on the Mir space station will then move the module to a radial port of the CCM.

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.

Dimensions

The length of each module is 14.4m. They are cylindrical with a maximum diameter of 4.2m and an on orbit mass between 20 and 22 thousand kilograms apiece.

Launch

Both modules are due for launch after 2020, on Long March 5 from Wenchang Satellite Launch Center, into low Earth orbit 340 to 450 kilometers above the Earth at an orbital inclination of 42 to 43 degrees, in the centre of the Earth's thermosphere.[2]

References

  1. ^ Pietrobon, Steven (25 August 2018). "Chinese Launch Manifest". Retrieved 25 August 2018.
  2. ^ David, Leonard. "China Details Ambitious Space Station Goals". SPACE.com. Retrieved 2012-02-23.

External links

  • Chinese Space Agency website
Retrieved from "https://en.wikipedia.org/w/index.php?title=Laboratory_Cabin_Module&oldid=856440024"
This content was retrieved from Wikipedia : http://en.wikipedia.org/wiki/Laboratory_Cabin_Module
This page is based on the copyrighted Wikipedia article "Laboratory Cabin Module"; it is used under the Creative Commons Attribution-ShareAlike 3.0 Unported License (CC-BY-SA). You may redistribute it, verbatim or modified, providing that you comply with the terms of the CC-BY-SA