The Orlan-MKS is a Russian spacesuit that cosmonauts wear for spacewalks at the International Space Station. NPP Zvezda and Roscosmos make it, and it has been in use there since 2017. The suit is semi-rigid, with a solid torso and flexible arms, and it carries its own life support in a backpack on the rear hatch.
The torso is a single hard shell, said to be an aluminium alloy. The pressure layer is polyurethane, which replaces rubber and, according to one report, makes the suit last longer. The outer fabric is phenylon, an aramid fibre.
Application
Used by cosmonauts for spacewalks on the International Space Station since 2017. The suit is self-contained, carrying its own life support in a rear hatch backpack, and is built for 15 to 20 EVAs.
Photos
How it is built
Hard torso and helmet
The hard upper torso, or cuirass, is a single shell said to be an aluminium alloy. The suit is entered through a rear hatch, which also carries the life support backpack. One blog reports that the helmet is impact-resistant polycarbonate.
Hard upper torso (cuirass)
Helmet
Pressure layer
In the new model, polyurethane pressure shells take the place of rubber ones. A Russian news report says this lengthens the suit's service life. The shells form the pressure bladder, the sleeves and the legs.
Pressure bladder, sleeves and legs
Outer fabric and heat control
The outer shell of the suit is phenylon, a fabric made from aramid, a family of strong synthetic fibres. For thermal insulation the suit has layers of aluminium foil and mineral fibres. Its thermal control system is fully automated, with a manual override.
Outer shell fabric
Thermal insulation
Where the parts areNumber of parts we have listed in each group
Layered thermal insulation. The description may cover the whole Orlan family rather than this model alone.
The materials by familyHow many of the parts that name a material use each one
Other15
Polymers and foams4
Aluminium3
Stainless steel2
Gold and silver1
Glass fibre1
How it connects to other things
Orlan is a family of Russian spacesuits, and the Orlan-MKS is a newer model of it. One change reported from earlier models is that polyurethane pressure shells replace rubber ones.
Used in
International Space Station, Russian segment EVA equipment (used from its airlocks)
Suits live on the station and are discarded with Progress, not returned
Builds on
Orlan-M spacesuit
Via the Orlan-MK, which can run as the earlier Orlan-M version
Orlan-DMA spacesuit
Indirect: Orlan-M, base of the MK and MKS, was an Orlan-DMA modification
Krechet lunar spacesuit (semi-rigid concept)
Semi-rigid Orlan family traces to the lunar programme suit
Replaces
Orlan-MK spacesuit
Replaced the Orlan-MK on the ISS; new polyurethane shell and automatic cooling
AluminiumTempered steel wire frame and steel-ring wrist hinge
Where each one is used
Aluminium. Here: Hard upper torso (cuirass); Rigid backpack (satchel) shell. There: Radial beams; Crushable ribs (x4) and more.
Tempered steel wire frame and steel-ring wrist hinge. Here: Glove palm frame and wrist hinge (Orlan-M design); Main and backup oxygen tanks (BK-3 units: tank, valve and two-stage reducing valve). There: Crew couch frames (x3); Couch shock-attenuating struts (x8).
What we do not know
Public descriptions come from a blog and from news and magazine articles, not from NPP Zvezda or Roscosmos, and some may describe the Orlan suits in general rather than this model. The restraint layer, visor, boots and gloves have no published materials.
The detailed data
What is written above is built from these numbers and quotes. Each row links to the page it was taken from. Get all of it as JSON, or ask our MCP server.
Features
Semi-rigid suit with a solid torso and flexible arms, rear hatch entry
Fully automated thermal control system with manual override
Polyurethane pressure shells replace rubber to extend service life
Specifications
What
Value
Mass
110 kg (240 lb)
Mass (Roscosmos-linked press)
about 110 kg
Operating pressure
400 hPa (5.8 psi); about 0.4 atm
Primary life support
7 hours
Service life
6 years; 15 to 20 EVAs
In service
ISS, since 2017
Cosmonaut height range
165 to 190 cm
Heat removal capacity
Average 300 kcal/h; maximum 600 kcal/h
EVA length quoted by RussianSpaceWeb
Up to nine hours
Backup pressure layer
Dropped on the MKS because the polyurethane layer resists failure
Polyurethane layer origin
Reportedly bought in Belgium (supplier not named)
Hermetic shell temperature range (No. 6)
-150 C to +120 C
ASTR water inlet and gas temperature ranges
Water 5 to 30 C; suit gas held at 5 to 20 C
ASTR first use
EVAs 43, 44, 45 and 46 from the Russian segment
Peak body heat output
Up to 800 W during hard work
Self-entry time (Orlan-M manual)
2 to 3 minutes without assistance
Cuirass alloy named for the Orlan family
AMg-3 aluminium alloy (family-level statement, not MKS-specific)
Deliveries
No. 6 on Progress MS-30 (28 Feb 2025); No. 7 on Progress MS-32 (11 Sep 2025); No. 8 on Progress MS-34 (April 2026)
Fleet rule
Three suits kept on the station: two main and one reserve
Replacement price (July 2021)
About 370 million rubles
Possible future upgrades
Jet-propelled rescue system and helmet-projected display (Zvezda, 2018)
Materials in detail
Each material named in the sources: where it is used here, which other products use it, and its key numbers when its material page exists.
Torso, pressure layer, outer fabric and insulation materials come from secondary or popular sources; no manufacturer datasheet found. Components, suppliers and links were added from public sources. A material is left blank where no source states it.
Natural rubber main shell, about 0.6 mm (Orlan-M)natural-rubber
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Glove palm frame and wrist hinge (Orlan-M design)Steel wire palm frame and steel-ring wrist hinge that give wrist bending and a concave palm“The frame is made of tempered steel wire”
Tempered steel wire frame and steel-ring wrist hinge (grade not stated)steel-grade-unstated
Main and backup oxygen tanks (BK-3 units: tank, valve and two-stage reducing valve)Two gaseous-oxygen units in the backpack; the manual describes 2-litre tanks at up to 420 kgf/cm2“Operational pressure in the main and backup oxygen tanks”
Steel alloy housing with fiberglass braiding (Orlan-M)steel-grade-unstated
Lithium hydroxide CO2 absorber with a kupramite contaminant layer (Orlan-M)lithium-hydroxide-co2-absorber
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Ventilation fans (main and backup, brushless motors)Circulate suit gas through the absorber and sublimator; the backup starts automatically if the main fails“The system uses two fans, a main and a backup.”
Rubberized fabric tank shell (Orlan-M); polyethylene foam filter elementrubberized-fabric
—
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Water circulation pumps (main and backup, centrifugal)Circulate cooling water through the garment; the pumps sit in the backpack“В ранце находятся насосы.”
ASTR automatic thermal-control valves (x2: heat-exchanger line normally closed, bypass normally open)Two solenoid valves that route water to or around the sublimator according to the wearer's estimated energy use“Исполнительными агрегатами являются два электромагнитных клапана”
No NPP Zvezda or Roscosmos primary document with layer materials was reachable. The aluminium-alloy torso claim comes from a single blog (newspaceeconomy.ca) and a general Russian article that does not name the suit; alloy not named. The phenylon fabric and foil/mineral-fibre insulation quotes come from a Vokrug Sveta article that may describe the Orlan family generally. Polycarbonate helmet is from the blog only. Restraint layer, visor, boots, gloves not sourced. Wikipedia lists 110 kg for MKS. More detail: No NPP Zvezda or Roscosmos engineering drawing or bill of materials for the Orlan-MKS itself is public. Most component detail comes from the 1998 Orlan-M cosmonaut training manual (Star City, English translation), the Orlan-MK press articles and a few MKS-specific items (ASTR thermal control papers, NPP Zvezda page, TASS and RussianSpaceWeb); rows are tagged Orlan-M, Orlan-MK or MKS accordingly, and the MKS may differ in detail (for example the MKS reportedly dropped the backup pressure layer, and gloves and shells moved from rubber to polyurethane). Not found: battery chemistry and maker, camera and display makers (the display is only called Russian-made), glove heaters (none described), the polyurethane supplier (only 'Belgium'), the structure of the MKS pressure layer beyond 'polyurethane', and any supplier of the radio, pumps, fans or valves. The Pozdnyakov TASS interviews were read only through English translations on suzymchale.com. The Roscosmos 2012 page copy had broken text encoding, so the Vesti.ru copy of the same story was used. No source gave a fit with the NASA EMU as an 'alternative' relation type, so none was added. Some quoted secondary sources (RussianSpaceWeb, Naked Science, 1ru) are press articles, not engineering documents; newspaceeconomy.ca was not used for new rows because it states lithium-ion batteries and Kevlar layers that no primary source confirms.