// RU-007 · Soviet / Russia

Sokol KV-2

Zvezda · 1980–present
IVA Active
Sokol KV-2 spacesuit

Technical Specifications

Pressure400 hPa
Suit mass (1g)TBD
Life support (primary)Vehicle-supported open-loop
Life support (backup)Emergency oxygen
EVA durationN/A
ProgramSoyuz
AgencyRoscosmos
ManufacturerZvezda
First use1980
StatusActive
Donning / entrySoft rescue suit with refined lower torso and closure logic; sea survival collar

Engineering Analysis

Key Subsystem Architecture

Long-lived Soyuz rescue standard; manufacturing continued into ISS era

Mission Role

Soyuz-T / TM / TMA / MS ISS ferry rescue standard

Limitations & Failures

Difficult donning; poor downward visibility; under-knee discomfort; decades of upgrade latency

Program Lesson
"Keep rescue-suit platforms on a managed block-upgrade path instead of deferring subsystem refresh for decades"
Future Relevance

Still flying today on Soyuz. Long-service record reveals both resilience and the cost of deferred modernisation

Documented Failure Cases
Medium 2026

Difficult donning, restricted downward vision, under-knee discomfort, appendix tie-off burden across decades of operations

→ IVA rescue suits fail operationally when crew usability is treated as secondary. Track don/doff time and visibility as design KPIs

// 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"

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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"

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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"

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