Artemis II Pre-Launch System Verification

Comprehensive Checkpoint for Crew Safety & Mission Success

0%

Total Checks

20

System Verifications

Personnel Required

12

Specialized Team Members

Safety Status

GO

Systems Ready

Propulsion Systems
Engine Gimbal Test: ±10 degrees operational range
Propellant Leak Detection: Zero detectable leaks
Thrust Chamber Pressure: ±5% of nominal tolerance
Valve Operation Test: <2 seconds response time
Fuel Temperature Monitoring: Within specified range

Responsible Personnel:

Propulsion Engineer Systems Engineer Safety Officer
Life Support Systems
Cabin Pressure Test: 14.7 ± 0.2 psi
Oxygen Concentration: 21-23% concentration
CO2 Removal Efficiency: >95% efficiency
Water Purification Cycle: <10 ppm contaminants
Fire Sensor Calibration: <1 second detection

Responsible Personnel:

Life Support Engineer Medical Officer Systems Technician
Navigation & Communication
GPS Constellation Lock: 4+ satellites locked
Star Tracker Calibration: 3+ stars identified
Communication Link Test: BER < 10^-6
Data Transmission: >1 Mbps downlink
Antenna Deployment Test: Full deployment confirmed

Responsible Personnel:

Navigation Engineer Communication Specialist Ground Controller
Safety Mechanisms
Abort Motor Readiness: <1 second activation
Egress Pathway Clear: <2 minutes to safe zone
Range Safety Command: Command authority verified
Debris Field Analysis: Safe trajectory maintained
Radiation Sensor Calibration: Below threshold limits

Responsible Personnel:

Safety Officer Range Safety Controller Medical Team

Interactive System Verification

Click to simulate verification of each system component