Engineering Archive · thespacesuits.com

THE
SUIT
ARCHIVE

Seventy years of pressure garment engineering across US, Soviet, Russian and incoming Chinese programs. Every variant. Every subsystem. Every failure. Primary sources—not Wikipedia summaries.

18+
Variants
16
Subsystems
16+
Failures
70yr
History
US Mercury IVA · X-15 · Gemini G3C · G4C · G5C · Apollo A7L · A7LB · Skylab · EMU · ACES · Enhanced EMU · xEMU · AxEMU SOVIET/RU SK-1 · SK-2 · BERKUT · YASTREB · KRECHET · SOKOL-K · SOKOL-KV-2 · ORLAN-D · ORLAN-DM · ORLAN-DMA · ORLAN-M · ORLAN-MK · STRIZH CHINA Shenzhou IVA · Haiying · Feitian Gen-1 · Feitian Gen-2 · Feitian D/E · Wangyu Lunar Suit EUROPE/ESA EVA Suit 2000 · EuroSuit IVA · Hermes EVA Concept US Mercury IVA · X-15 · Gemini G3C · G4C · G5C · Apollo A7L · A7LB · Skylab · EMU · ACES · Enhanced EMU · xEMU · AxEMU SOVIET/RU SK-1 · SK-2 · BERKUT · YASTREB · KRECHET · SOKOL-K · SOKOL-KV-2 · ORLAN-D · ORLAN-DM · ORLAN-DMA · ORLAN-M · ORLAN-MK · STRIZH CHINA Shenzhou IVA · Haiying · Feitian Gen-1 · Feitian Gen-2 · Feitian D/E · Wangyu Lunar Suit EUROPE/ESA EVA Suit 2000 · EuroSuit IVA · Hermes EVA Concept
18
US Program Variants
Mercury through AxEMU. 18 operational and reference variants spanning IVA, IEVA, and orbital EVA systems.
17
Soviet / Russian Suits
SK-1 to Orlan-MK. Rescue IVA, lunar EVA concepts, and the rear-entry Orlan family still operating on the ISS today.
50+
Failure Modes Logged
Hard failures, near-misses, chronic constraints. Includes EVA-23 — the helmet water intrusion that nearly killed Luca Parmitano.
4
China & Europe Now Live
6 Chinese suits from Shenzhou IVA through Wangyu lunar suit. Plus ESA EVA Suit 2000 and EuroSuit IVA tested on ISS by Sophie Adenot in 2026.
// Variant Master Database

Featured Suits

Normalized across pressure, mass, life support, mission role and failure modes

View All 18 Suits →
VAR-001 IVA
Mercury IVA spacesuit photograph

Mercury IVA

NASA · B.F. Goodrich
1959–1963
Pressure
3.7 psi / 25.5 kPa
System mass
22 lb
Life support
Vehicle provided
EVA duration
N/A

"Even a simple IVA suit needs water survival and cockpit visibility contingencies"

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VAR-004 IEVA
Gemini G4C + VCM spacesuit photograph

Gemini G4C + VCM

NASA · David Clark + AiResearch
1964–1965
Pressure
3.7 psi / 25.5 kPa
System mass
41.75 lb (system)
Life support
VCM umbilical / vehicle-fed purge
EVA duration
N/A

"Suit performance cannot be separated from translation aids and workload planning"

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VAR-008 IEVA
Apollo A7L + PLSS-6 spacesuit photograph

Apollo A7L + PLSS-6

NASA · ILC Industries + Hamilton Standard
1966–1971
Pressure
3.7 psi / 25.5 kPa
System mass
201 lb (system)
Life support
PLSS-6 nominal 6 hr
EVA duration
6 hours

"Lunar EVA required not just survival but sustained human work capability"

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VAR-009 IEVA
Apollo A7LB + PLSS-7 spacesuit photograph

Apollo A7LB + PLSS-7

NASA · ILC Industries + Hamilton Standard
1968–1975
Pressure
3.7 psi / 25.5 kPa
System mass
212 lb (system)
Life support
PLSS-7 nominal 7 hr
EVA duration
7 hours

"Endurance and traversal demands exposed the need for mobility, dust robustness, and rover integration"

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VAR-012 EVA
Shuttle Baseline EMU spacesuit photograph

Shuttle Baseline EMU

NASA · Hamilton Standard + ILC
1976–2002
Pressure
4.3 psi / 29.6 kPa
System mass
254 lb (system)
Life support
PLSS nominal 8 hr
EVA duration
8 hours

"Dedicated EVA architecture dramatically improved work efficiency vs IEVA"

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VAR-015 EVA

Enhanced EMU

NASA · Hamilton Sundstrand + ILC
1990–present
Pressure
4.3 psi / 29.6 kPa
System mass
309 lb (system)
Life support
PLSS 8 hr; regenerative CO2 removal
EVA duration
8 hours

"Long-life EVA programs shift from design problems to sustainment, anomaly and industrial-base problems"

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// Engineering Deep-Dive

WHY GLOVES
KEPT KILLING
EVERY MISSION

Across 70 years and three space programs, the same subsystem remained the single most persistent mission limiter: the glove. Hand fatigue in Gemini IV made America's first EVA nearly catastrophic. Cold-object handling plagued Apollo. Pre-Phase VI EMU glove injuries—numbness, bladder bunching, palm-bar wear-through into hand—drove formal NASA injury surveillance in the 1990s.

The archive documents 12 distinct glove development lines across US and Soviet programs. Not what was built—but why each iteration failed to solve the fundamental physics of dexterity under 3.7–5.8 psi. The Russian BERKUT glove of 1965 and the ISS Phase VI of 2002 share the same core failure: torque and thermal performance trade against each other at the finger joint level.

Read Subsystem Analysis
Rear Entry
Why Soviets Chose Rear-Entry Architecture

KRECHET-94 and the Orlan family both use rear-entry hard upper torso. Not accidental — it solved donning alone on a lunar surface without ground crew. Traced from 1967 through modern suitport concepts.

Explore KRECHET →
Critical Failure
EVA-23: Helmet Water Intrusion

2013. ISS. Parmitano's helmet filled with water. Vision impaired, comms degraded, breathing compromised. Water separator blockage in the enhanced EMU's cooling loop. Potentially lethal. Full forensic breakdown here.

Read Failure Case →
Coming Soon
China Feitian Workbook

Third major space power's EVA program documented in the same structured engineering format as US and Soviet workbooks. Feitian EVA suit subsystem decomposition and roadmap. Imminent.

Get notified →
// What Actually Broke

Critical Failures

No euphemisms. Sourced from NASA, OIG reports, and Soviet technical archives.

All 16 Failure Cases →
Critical 2026
ISS Enhanced EMU — EVA-23
Life support / water loop

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

Critical 2026
Enhanced EMU Sustainment
Program / industrial base

Aging suits, obsolescence, contractor quality issues, supply-chain weaknesses — OIG 2025 flagged as mission risk

→ Industrial-base fragility becomes a technical failure mode in long-lived fleets. Supplier resilience must be a first-class design and program requirement

Critical 2026
xEMU Program
Mass / program integration

Suit mass exceeded or stressed downstream lander allocations; requirements breadth and subsystem mass growth degraded feasibility

→ Exploration programs need firm mass control and stable mission assumptions before subsystem elaboration begins. Lock the budget model early

Critical 2026
Pure oxygen atmosphere
Atmosphere / materials

High-pressure pure oxygen atmosphere drastically increased flammability and toxicity consequences

→ Atmosphere, materials, and operations must be treated as a single integrated safety system from day one

50+Variants Documented
16Subsystems Analyzed
50+Failure Cases Logged
70yrTimeline Coverage
4Nations — US · Soviet · China · ESA
// Why This Archive Exists

ENGINEERED HERE.
NOT
GENERATED.

Sixty years of pressure garment failures, near-misses and hard lessons — documented from primary sources. NASA technical reports, OIG audits, Zvezda records. The kind of archive that takes months to build and seconds to trust.