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Soyuz MS-14 Uncrewed

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Overview

Destination: Low Earth Orbit
Mission: Resupply

Low Earth Orbit 31/6 Baikonur Cosmodrome, Republic of Kazakhstan

Uncrewed Soyuz MS spacecraft to bring cargo to the space station. This demo flight tests a modified motion and navigation control system, as well as mating to Soyuz-2.1a rocket. The results will be used in development of an uncrewed cargo vehicle, based on Soyuz spacecraft.

Soyuz 2.1a

Family:
Configuration:

The Soyuz 2.1A converted the flight control system from analog to digital, which allowed launch from fixed platforms. It also allowed big fairings and payloads. It is currently used for crewed Soyuz and Progress flights to the ISS.

Specifications
  • Minimum Stage
    2
  • Max Stage
    3
  • Length
    46.3 m
  • Diameter
    2.95 m
  • Fairing Diameter
  • Launch Mass
    312.0 T
  • Thrust
    4149.0 kN
Family
  • Name
    Soyuz 2.1a
  • Family
  • Variant
  • Alias
  • Full Name
    Soyuz 2.1a
Payload Capacity
  • Launch Cost
    $80000000
  • Low Earth Orbit
    7020.0 kg
  • Geostationary Transfer Orbit
    2810.0 kg
  • Direct Geostationary
  • Sun-Synchronous Capacity
    4230.0 kg

Soyuz MS-14


Active Human Rated Unmanned Crew Capacity: 3
Destination: International Space Station
Serial Number: Soyuz MS 11F732A48 #743

Soyuz MS-14 is an unmanned flight of the Soyuz spacecraft intended to test a modification for the Launch Abort System.

Soyuz MS Details

Progress Rocket Space Center

Progress Rocket Space Center

(PRSC)

CEO: Dmitry Baranov Founded: 1996 Successes: 44 Failures: 1 Pending: 0

Agency Type:

Progress Rocket Space Centre, formerly known as TsSKB-Progress, is a space science and aerospace research company which is known for manufacturing launch vehicles and satellites. Most notably, Progress Rocket Space Centre is the manufacturer of Soyuz launch vehicles.

INFO WIKI

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