// VAR-012 · United States

Shuttle Baseline EMU

Hamilton Standard + ILC · 1976–2002
EVA Retired / evolved
Shuttle Baseline EMU spacesuit

Technical Specifications

Pressure4.3 psi / 29.6 kPa
Suit mass (1g)254 lb (system)
Life support (primary)PLSS nominal 8 hr
Life support (backup)Secondary oxygen package 30 min
EVA duration8 hours
ProgramShuttle
AgencyNASA
ManufacturerHamilton Standard + ILC
First use1983
StatusRetired / evolved
Donning / entryRear-entry modular HUT/LTA architecture

Engineering Analysis

Key Subsystem Architecture

Hard torso, bearings, replaceable modules, MMU/SAFER compatibility

Mission Role

Orbital assembly, repair, servicing — Shuttle era

Limitations & Failures

Massive at 1g; glove/cold-object issues; maintenance burden

Program Lesson
"Dedicated EVA architecture dramatically improved work efficiency vs IEVA"
Future Relevance

Core template for ISS and exploration EVA systems — direct ancestor of AxEMU

Documented Failure Cases
High 1965

First US EVA physically exhausting and low-productivity despite suit functioning; glove productivity inadequate for task completion

→ Suit capability and worksite design must be developed together, not sequentially

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

High 1980s–1990s

Numbness, bladder bunching, and palm-bar wear-through into hand across multiple crew members

→ Glove verification must include extended-use comfort and injury surveillance, not just pressure integrity and cold-object performance

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

// Related Suits

Same Program Family

PROTO-001 Prototype EXPERIMENTAL
Mk II Model O spacesuit photograph

Mk II Model O

USAF · B.F. Goodrich
1956
Pressure
TBD
System mass
TBD
Life support
Not publicly documented
EVA duration
N/A

"Established B.F. Goodrich as the lead US full-pressure suit contractor before Mercury existed"

View Full Archive →
PROTO-002 Prototype EXPERIMENTAL
Mk II Model R spacesuit photograph

Mk II Model R

USAF · B.F. Goodrich
1956
Pressure
TBD
System mass
TBD
Life support
Not publicly documented
EVA duration
N/A

"Parallel development track alongside Model O testing different mobility solutions"

View Full Archive →
PROTO-003 Prototype EXPERIMENTAL
Mk IV Arrowhead spacesuit photograph

Mk IV Arrowhead

US Navy · B.F. Goodrich
late 1950s
Pressure
TBD
System mass
TBD
Life support
Not publicly documented
EVA duration
N/A

"Naval and NASA pressure suit research tracks cross-pollinated significantly in this era"

View Full Archive →