// RU-010 · Soviet / Russia

Orlan-M

Zvezda · 1997–present
EVA Active lineage

Technical Specifications

Pressure5.8 psi / 40 kPa
Suit mass (1g)238 lb
Life support (primary)Self-contained 100% O2 — 7 hr
Life support (backup)Integrated reserve / vehicle procedures
EVA duration7 hours
ProgramMir / ISS
AgencyRoscosmos
ManufacturerZvezda
First use1997
StatusActive lineage
Donning / entrySemi-rigid rear-entry integrated body/helmet; on-board drying and recharge ecosystem

Engineering Analysis

Key Subsystem Architecture

Higher pressure reduces prebreathe burden; comparison with DMA shows HUT/backpack evolution; BSS station interfaces

Mission Role

Station EVA — Russian ISS segment operations

Limitations & Failures

Storage/humidity control; consumables; refurbishment cadence; interface non-trivial with US segment

Program Lesson
"Orbital EVA systems must be treated as maintainable fleets, not isolated suits"
Future Relevance

Still operating on ISS. Fleet-maintenance lessons directly inform all next-generation EVA design

Documented Failure Cases
High 1960s

Unexpected arm growth when shoulder restraint cable failed; seized pulley caused overheating in crotch-thigh region

→ Critical restraint paths need redundancy or condition monitoring. Small mechanical hardware in pressure-load paths creates outsized crew risk

High 1965

Suit inflation during Leonov's EVA made movement and airlock re-entry critically difficult — Leonov had to partially deflate to re-enter

→ Make ingress/egress and self-rescue a separate verification gate from EVA capability itself

Critical 2013

Water entered Luca Parmitano's helmet during EVA — vision impaired, comms degraded, breathing compromised

→ Cooling-water management is a primary safety-critical function, not a nuisance issue. Contamination tolerance must be designed in from day one

Medium 1977–

Repeated orbital use shifted primary risk toward maintenance, drying, recharge, and replaceable component management

→ Not all critical failures are dramatic punctures. Slow fleet degradation from poor maintenance design matters as much as acute failures

// Related Suits

Same Program Family

RU-001 IVA
SK-1 / SK-2 spacesuit photograph

SK-1 / SK-2

Soviet Space Program · Zvezda
1961–1963
Pressure
300 hPa
System mass
TBD
Life support
Vehicle-supported open-loop + post-ejection oxygen
EVA duration
N/A

"Shows value of integrated survival architecture and the penalty of long-duration IVA wear in a rigidly seated posture"

View Full Archive →
RU-002 EVA

BERKUT

Soviet Space Program · Zvezda
1965
Pressure
400 hPa
System mass
TBD
Life support
Open-loop backpack KP-55 oxygen
EVA duration
N/A

"Pressurized mobility and re-entry-to-airlock recovery must be a top-level requirement, not an afterthought"

View Full Archive →
RU-005 EVA

KRECHET

Soviet Space Program · Zvezda
1967–1972
Pressure
400 hPa
System mass
TBD
Life support
Self-contained backpack + lunar interfaces
EVA duration
N/A

"Rear-entry and semi-rigid architecture remain highly relevant for surface systems and suitport concepts"

View Full Archive →