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Soyuz TMA-M

Soyuz TMA-M

Spaceships
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Basic Information
Name
Soyuz TMA-M
Designation
Soyuz TMA-M
Alternate Designation
Equipment Type
Spaceships
Manufacturer
Rocket and Space Corporation Energia
Date of Introduction
2011
Description

The Soyuz TMA-M is an upgraded version of Soyuz TMA slated to enter service after 2010 replacing its predecessor carrying out space manned flights in support of the Russian Federal Space Agency. The spaceship's construction process has been improved to make it easier to manufacture. The Soyuz TMA-M will feature digital interior displays and updated docking equipment as well as the ability to stay in space for one year compared to six months for the Soyuz TMA spacecraft as well as increased payload through mass reduction of the onboard systems. Three flights have been scheduled to validate the design of the new Soyuz starting on October 8, 2010 with a flight to the International Space Station (ISS). The first two flights are development tests with the third flight planned as a qualification test. The Soyuz TMA-M has replaced the onboard devices of guidance, navigation and control system (GN&CS) and onboard measurement system (OMS) by the devices developed on the basis of modern EEE parts and matured software. It also extends the functional capabilities of the vehicle with regard to the onboard system control from the onboard computers of GN&CS and provide deeper integration with the onboard computers of the International Space Station Russian Segment (ISS RS) when using a multiplex exchange channel. The electric power consumption has been also reduced dramatically. The temperature control equipment has also been updated. Externally, the new Soyuz keeps the same configuration of the TMA version. All in 36 obsolete devices were replaced by 19 new devices decreasing the vehicle's structure mass by 70 kg.

Air & Air Defense Specifications
Crew 3
Overview (Deagel)
Group Spaceships
Status Retired - No Longer Operational
Origin Russia
Contractor Rocket and Space Corporation Energia
Initial Operational Capability (IOC) 2011
First Flight October 8, 2010
Total Production 20
Specifications (Deagel)
Crew 3
Dimensions — Cabin Width 2.2 meter
Dimensions — Diameter 2.7 meter
Dimensions — Length 7.0 meter
Dimensions — Solar Panel Span 10.7 meter
Mass — Max Landing Weight 2,900 kilogram
Mass — Max Takeoff Weight 7,220 kilogram
Mass — Payload 170 kilogram
Performance — Orbit 460 kilometer
Time — Mission Endurance 360 day
Time — Service Life 360 day
Variants
Variant 1 Soyuz TMA
Variant 2 Soyuz TMA-M
Variant 3 Soyuz TMA-MS
Details
Country of Origin Russia
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
7 m
Width
2.7 m
Height
Weight
2900 kg
Operators (1)
Russia
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