// CN-002 · China / CMSA

Feitian Gen-1

CASC · 2008
EVA Retired

Technical Specifications

Pressure400 hPa
Suit mass (1g)TBD
Life support (primary)Self-contained EVA backpack oxygen
Life support (backup)Airlock support
EVA durationN/A
ProgramVoskhod / Shenzhou VII
AgencyCMSA / CNSA
ManufacturerCASC
First use2008
StatusRetired
Donning / entryOrlan-influenced semi-rigid rear-entry EVA architecture

Engineering Analysis

Key Subsystem Architecture

Fire and radiation-resistant materials; domestic sovereign EVA baseline; ~30m RMB cost reported

Mission Role

China's first domestic EVA — Zhai Zhigang, Shenzhou VII 2008

Limitations & Failures

Limited operational cadence; not a mature fleet product; imported Haiying suit flew alongside as backup

Program Lesson
"Pragmatic dual-track approach — import to reduce mission risk while demonstrating domestic capability simultaneously"
Future Relevance

Validates China's sovereign EVA technology transition path; Feitian Gen-1 is to China what BERKUT was to the Soviets

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

High 2024–

Risk that Feitian Gen-2 orbital EVA success may drive incremental adaptation to lunar surface rather than treating Wangyu as a new architecture branch

→ Orbital EVA success is not a sufficient baseline for lunar surface operations — treat as a new product architecture, not an upgrade

Medium 2021–

Suit lifespan initially limited to 15 EVAs over 3 years; exceeded in operations before upgrade to 20 EVAs/4 years D/E series

→ Track cost-per-EVA, turnaround time and anomaly-free hours as primary KPIs once a suit enters fleet operations

// Related Suits

Same Program Family

CN-001 IVA

Shenzhou IVA / Rescue Suit

CMSA / CNSA · CASC
2003–present
Pressure
TBD
System mass
TBD
Life support
Vehicle oxygen + emergency tanks
EVA duration
N/A

"Rescue suit discipline must be kept separate from EVA product line — do not overbuild IVA with EVA objectives"

View Full Archive →
CN-003 EVA

Feitian Gen-2 Tiangong

CMSA / CNSA · CASC
2021–present
Pressure
TBD
System mass
287 lb
Life support
Backpack PLSS — liquid cooling, oxygen, humidity, telemetry
EVA duration
7 hours

"Once a suit becomes a fleet asset, lifecycle economics and telemetry matter more than peak performance figures"

View Full Archive →
CN-004 EVA

Wangyu Lunar Suit

CMSA / CASC · CASC
2024–2030
Pressure
TBD
System mass
TBD
Life support
Self-contained lunar PLSS (details not public)
EVA duration
N/A

"Lunar suit must be treated as a new architecture branch — not an incremental Feitian derivative — due to dust, terrain and thermal differenc…"

View Full Archive →