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Soyuz MS
Latest revision of the Soyuz spacecraft From Wikipedia, the free encyclopedia
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The Soyuz MS (Russian: Союз МС; GRAU: 11F732A48) is the latest version of the Russian Soyuz spacecraft series, first launched in 2016. The "MS" stands for "modernized systems," referring to improvements in navigation, communications, and onboard systems over the Soyuz TMA-M series. Developed and manufactured by Energia, it is operated by Roscosmos for human spaceflight missions to the International Space Station (ISS).
Soyuz MS-01, the first flight of the series, launched on 7 July 2016 and docked with the ISS two days later following a checkout phase to validate the new systems. The mission lasted 113 days, concluding with a landing on the Kazakh Steppe on 30 October 2016.
The Soyuz MS spacecraft has been involved in one in-flight abort. During the launch of Soyuz MS-10 in October 2018, a booster separation failure on the Soyuz-FG launch vehicle triggered the automated launch escape system. The spacecraft separated from the rocket and returned the crew safely to Earth under parachutes. The crew landed unharmed. Since April 2020, the spacecraft has been launched using the modernized Soyuz 2.1a rocket.
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Design
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Like earlier versions of the Soyuz, the MS spacecraft variant consists of three sections (from forward to aft in orbit, or top to bottom when mounted on a rocket):
- A spheroid orbital module
- A small aerodynamic descent module
- A cylindrical instrumentation and propulsion module
The orbital and descent modules are pressurized and habitable. By relocating much of the equipment and usable volume to the orbital module—which does not require heat shielding for atmospheric re-entry—the three-part Soyuz design is both larger and lighter than comparable two-part spacecraft. For comparison, the Apollo spacecraft's pressurized command module provided a crew of three with six cubic metres (210 cu ft) of living space and had a re-entry mass of approximately 5,000 kilograms (11,000 lb), while the Soyuz MS offers the same crew ten cubic metres (350 cu ft) of living space with a re-entry module mass of about 2,950 kilograms (6,500 lb).
The Soyuz MS can carry up to three crew members and supports free-flight missions lasting approximately 30 person-days. Its life support system provides a nitrogen–oxygen atmosphere similar to that of Earth, with air pressure equivalent to sea level. Oxygen is regenerated using potassium superoxide (KO2) canisters, which absorb most of the carbon dioxide (CO2) and water exhaled by the crew and release oxygen. Lithium hydroxide (LiOH) canisters are also used to absorb residual CO2.
In addition to the crew, Soyuz MS can carry up to 200 kilograms (440 lb) of payload to orbit and return up to 65 kilograms (143 lb) to Earth.[1]
The spacecraft is protected during launch by a nose fairing with a launch escape system, which is jettisoned once the vehicle exits the dense layers of the atmosphere. Soyuz MS is highly automated; its Kurs system enables automatic rendezvous and docking with the ISS. Manual control is possible in the event of system failure.
Orbital module

The forward-most section of the spacecraft is the orbital module (Russian: Бытовой отсек (БО), romanized: Bitovoy Otsek (BO), or habitation module). It provides more living space than the descent module and includes a toilet.
It has three hatches: a forward hatch for docking with the ISS, a side hatch for crew ingress and egress during ground operations, and an aft hatch connecting to the descent module. In principle, the side hatch could be used for spacewalks by sealing the other hatches and using the module as an airlock, although this capability has never been used on the MS variant due to the availability of larger dedicated airlocks on the ISS.
In microgravity, the orbital module's conceptual orientation differs from that of the reentry module, with crew members positioned with their heads toward the forward docking port. A small forward-facing window allows the flight engineer to visually assist the commander—who pilots the spacecraft from the reentry module—during manual docking if the automated system fails.
The module can accommodate over 100 kilograms (220 lb) of cargo at launch and is typically filled with up to 170 kilograms (370 lb) of waste before being jettisoned prior to re-entry where it will burn up in the atmosphere.
The orbital module can be customized for specific mission requirements without affecting the safety-critical systems of the descent module. Compared to earlier Soyuz versions, it incorporates additional anti-meteoroid shielding.[2]
Descent module

The central section is the descent module (Russian: Спускаемый аппарат (СА), romanized: Spuskaemiy Apparat (SA)), which houses the crew during launch and return. During re-entry it is shielded by a heat-resistant covering and slowed using atmospheric drag and parachutes. At one metre (3 ft 3 in) above ground, solid-fuel landing engines behind the heat shield fire to cushion the final impact.
The reentry module is designed for high volumetric efficiency (internal volume relative to hull surface area). A spherical shape would be optimal but offers no lift, resulting in a fully ballistic reentry, which is difficult to steer and subjects the crew to high g-forces. Instead, the Soyuz uses a compromise "headlight" shape: a hemispherical forward section, a shallow conical midsection, and a spherical heat shield, allowing limited lift and steering. The nickname derives from the resemblance to early sealed beam automotive headlights.
Instrumentation/propulsion module

The aft section is the instrumentation/propulsion module (Russian: Приборно-Агрегатный Отсек [ПАО], romanized: Priborniy-Agregatniy Otsek [PAO]), also referred to as the service module or aggregate compartment. It consists of three parts: the instrumentation compartment (Russian: Приборно Отсек [ПО], romanized: Priborniy Otsek [PO]), the instrumentation compartment (Russian: Приборно Отсек [ПО], romanized: Priborniy Otsek [PO]), and the propulsion compartment (Russian: Агрегатный Отсек [АО], romanized: Agregatniy Otsek [AO]).
The instrumentation compartment is a pressurized container housing systems for power generation, thermal control, communications, telemetry, and attitude control. The propulsion compartment contains the main and backup liquid-fueled engines for orbital maneuvers and deorbiting. Low-thrust attitude control thrusters are mounted on the intermediate compartment. Solar panels and orientation sensors are mounted externally on the service module.
Re-entry procedure

The Soyuz spacecraft initiates its return to Earth with a deorbit burn approximately half an orbit, or 180 degrees, ahead of the designated landing site. The spacecraft is oriented tail-first, and the main engine fires for about five minutes to reduce velocity and lower the orbit. This maneuver typically takes place as the vehicle passes over the southern tip of South America at an altitude of about 422 kilometres (262 mi).[3]
About 30 minutes after the deorbit burn, as the spacecraft passes over the Arabian Peninsula at an altitude of roughly 140 kilometres (87 mi), the three modules separate. Only the descent module, which carries the crew, is designed to survive reentry; the orbital and service modules burn up in the atmosphere. To ensure successful separation under all circumstances, the spacecraft uses a four-tiered backup system: two automated commands, a manual override, and an emergency thermal sensor triggered by rising reentry temperatures.[3]
The descent module reenters the atmosphere at an angle of approximately 1.35°, generating some aerodynamic lift to reduce g-forces compared to a purely ballistic trajectory. In the event of flight control or attitude system failure, the capsule can revert to a ballistic descent, and crews are trained to withstand the higher loads associated with it.[3]
At around 100 kilometres (62 mi) altitude, atmospheric drag rapidly decelerates the spacecraft, and reentry heating causes the ablative outer layers of the shield to burn away. Plasma forms around the capsule, temporarily interrupting communications with ground stations. The onboard flight control system can adjust the capsule’s roll to fine-tune its trajectory.[3]
Parachute deployment begins at about 10 kilometres (6.2 mi) altitude. Two pilot chutes deploy first, followed by a drogue chute that slows the spacecraft from 230 to 80 metres per second (830 to 290 km/h; 510 to 180 mph), followed by the main parachute which further reduces the descent rate to 7.2 metres per second (26 km/h; 16 mph). At approximately 5.8 kilometres (3.6 mi) altitude, the heat shield is jettisoned, exposing the soft-landing engines, an altimeter, and a beacon light. Cabin pressure is gradually equalized with the outside atmosphere.[3]
At an altitude of about one metre (3 ft 3 in), the altimeter triggers the solid-fuel braking engines, reducing impact speed to under 2 metres per second (7.2 km/h; 4.5 mph). Each seat is equipped with shock absorbers and a liner custom molded to each crew member's body shape to cushion the final impact.[4] In the rare case of a landing under a backup parachute, descent speeds may reach 10.5 metres per second (38 km/h; 23 mph), but the descent module and seating systems are designed to remain survivable.[3]
After touchdown, the main parachute is released to prevent the capsule from being dragged by the wind. The module may land upright or on its side. Recovery beacons and transmitters activate automatically. If needed, the crew can manually deploy additional antennas. The spacecraft's autonomous navigation system (ASN-K) also transmits real-time position data via satellite to assist search and rescue operations.[3]
Soyuz landings are conducted in flat, open areas without major obstacles. Thirteen designated landing zones in Kazakhstan meet these criteria. Mission planners typically schedule landings during the spacecraft’s first or second orbit of the day, as it moves from south to north. Most landings occur at twilight, allowing recovery teams to visually track the brightly lit capsule against the darkening sky. Since Soyuz began servicing the ISS, only a few missions have landed at night.[5]
If the capsule lands in remote terrain far from the recovery teams, the crew has access to a portable survival kit. This includes cold-weather clothing, a medical kit, a strobe light, a handheld radio, a signal mirror, matches and firestarter, a fishing kit, and a semi-automatic pistol—intended for protection against wildlife such as wolves or bears.[6]
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Soyuz MS improvements
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The Soyuz MS includes a number of upgrades over the earlier Soyuz TMA-M variant:[7][8][9][10]
- Apparatus for Satellite Navigation (ASN-K, Russian: Аппаратура Спутниковой Навигации [АСН-К], romanized: Apparatura Sputnikovoi Navigatsii): Replaces ground-based tracking with the use of GLONASS and GPS signals. The system includes four fixed antennas and provides positional accuracy of 5 m (16 ft), with a design goal of 3 cm (1.2 in) and 0.5° attitude accuracy.[9]
- Kurs-NA rendezvous system: The Kurs-NA (Russian: Курс-Новая Активная, romanized: Kurs-Novaya Aktivnaya, lit. 'Course-New Active') docking system replaces the older Ukrainian-built Kurs-A system. Kurs-NA is 25 kg (55 lb) lighter, 30% smaller, and consumes 25% less power. It uses a single phased-array antenna instead of four directional antennas, while retaining and repositioning two narrow-angle antennas. An LED light also replaced the halogen docking light.[11][12]
- Unified Command and Telemetry System (EKTS, Russian: Единая Командно-Телеметрическая Система, romanized: Edinaya Komandno-Telemetricheskaya Sistema): Consolidates previous systems (BRTS, MBITS, Rassvet) into a single unit that supports satellite-based communication through Russia’s Luch relay system, providing coverage for up to 83% of each orbit. The spacecraft also retains VHF and UHF radios and can interface with U.S. TDRSS and European EDRS networks. A COSPAS-SARSAT transponder enables real-time location tracking during reentry.[13]
- Reconfigured attitude control thrusters: The Integrated Propulsion System (Russian: Комбинированная Двигательная Установка, romanized: Kombinirovannaya Dvigatelnaya Ustanovka [KDU]) uses two redundant manifold loops to supply fuel and oxidizer to 14 pairs of thrusters. Each pair connects to separate loops for redundancy. The number of aft-facing thrusters is doubled to provide backup for the main engine. The avionics and EFIR fuel-tracking unit are also redesigned to improve reliability.[14]
- Docking mechanism enhancements: The SSVP docking system includes a backup electric drive mechanism.[15]
- SZI-M reusable flight recorder: A ruggedized black box, the SZI-M (Russian: Система Запоминания Информации [СЗИ-М], romanized: Sistema Zapominaniya Informatsii, lit. 'Information Storage System'), is located beneath the commander's seat. It records voice and data throughout the mission, with a 4 GB capacity. It withstands impacts up to 150 m/s (490 ft/s) and temperatures up to 700 °C (1,300 °F) for 30 minutes and is rated for 100,000 overwrite cycles and up to ten reuse missions.[16][17]
- Power system upgrades: A fifth battery with a capacity of 155 Ah is added to support increased power demands. Solar cell efficiency increases from 12% to 14%, and panel surface area increases by 1.1 m2 (12 sq ft).[18]
- Enhanced micrometeoroid protection: Additional shielding is installed on the orbital module, primarily at NASA’s request, to reduce vulnerability to space debris and micrometeoroid impacts.[18]
- Digital camera system: The analog video system is replaced with an MPEG-2-based digital video system, enabling space-to-space RF communication with the ISS and reducing signal interference.[19]
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List of flights
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References
External links
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