Soyuz MS

Soyuz MS
Союз МС
Soyuz MS-20 approaching the ISS
ManufacturerEnergia
Country of originRussia
OperatorRoscosmos
Specifications
Spacecraft typeCrewed spaceflight
Launch mass7,080 kg (15,610 lb)
Crew capacity3
Volume10.5 m3 (370 cu ft)
Batteries755 Ah
RegimeLow Earth orbit
Design life210 days when docked to
International Space Station (ISS)
Dimensions
Solar array span
Width2.72 m (8 ft 11 in)
Production
StatusActive
Built24
Launched24 (as of 15 Sep 2023)
Operational2
Retired22 (not including MS-10)
Failed1 (Soyuz MS-10)
Maiden launchSoyuz MS-01
(7 July 2016)
Last launchActive
Related spacecraft
Derived fromSoyuz TMA-M
← Soyuz TMA-M Orel

The Soyuz MS (Russian: Союз МС; GRAU: 11F732A48) is a revision of the Russian spacecraft series Soyuz first launched in 2016. It is an evolution of the Soyuz TMA-M spacecraft, with modernization mostly concentrated on the communications and navigation subsystems. It is used by Roscosmos for human spaceflight. The Soyuz MS has minimal external changes with respect to the Soyuz TMA-M, mostly limited to antennas and sensors, as well as the thruster placement.[2]

The first launch was Soyuz MS-01 on 7 July 2016, aboard a Soyuz-FG launch vehicle towards the International Space Station (ISS).[3] The trip included a two-day checkout phase for the design before docking with the ISS on 9 July 2016.[4]

  1. ^ "Soyuz MS". Spaceflight 101.
  2. ^ Cite error: The named reference popularmechanics-20160705 was invoked but never defined (see the help page).
  3. ^ Cite error: The named reference tass-enscience886832 was invoked but never defined (see the help page).
  4. ^ Cite error: The named reference rsw-soyuzms01 was invoked but never defined (see the help page).