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Soyuz TMA

Soyuz TMA

Spaceships
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Basic Information
Name
Soyuz TMA
Designation
Soyuz TMA
Alternate Designation
Progress, Soyuz 7K-L3, Soyuz 7K-OK, Soyuz 7K-T, Soyuz 7K-TM, Soyuz A, Soyuz T, Soyuz TM
Equipment Type
Spaceships
Manufacturer
Rocket and Space Corporation Energia
Date of Introduction
2003
Description

The Soyuz TMA manned transport spacecraft derived from the Soyuz TM in accordance with intergovernmental agreements between Russia and the United States of America (USA). It is an integral part of the Orbital International Space Station (ISS) Complex providing rescue of the main crew of the station and delivering special visiting crews of up to three-man and small cargoes. Besides, Soyuz TMA spacecraft is also used for disposal of wastes from the station which are burned down in the atmosphere during descent. It is launched using the Soyuz FG rocket. As of August 2010, the Soyuz TMA program has involved 19 spacecrafts with the first 10-day mission test launch Soyuz TMA-1 on October 30, 2002, followed by the first flight mission by Soyuz TMA-2 on April 26, 2003. The Soyuz spacecraft consists of three modules: orbital module, descent module, and service module. The orbital module at the forefront of the spacecraft is designed to accommodate the crew during their mission in orbit. The descent module in the inner position is also habitable and is equipped with a heat shield, brake and main parachutes along with solid-fuel braking engines mounted behind the heat shield that ignite at 1 meter above the ground to accomplish the spacecraft's landing. The service module contains the engines, solar panels and instruments. Both the orbital and service modules are destroyed during the re-entry into the atmosphere.

Air & Air Defense Specifications
Crew 3
Overview (Deagel)
Group Spaceships
Status Retired - No Longer Operational
Also Known As Progress, Soyuz 7K-L3, Soyuz 7K-OK, Soyuz 7K-T, Soyuz 7K-TM, Soyuz A, Soyuz T, Soyuz TM
Origin Russia
Contractor Rocket and Space Corporation Energia
Initial Operational Capability (IOC) April 26, 2003
First Flight October 30, 2002
Total Production 21
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 100 kilogram
Performance — Orbit 460 kilometer
Time — Mission Endurance 200 day
Time — Service Life 200 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 (2)
Russia
United States
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