RADAR LOCK: ACQUIRED
DESCENT CAM: ACTIVE (24 FPS)
G-LOAD: 12.4 G
DESCENT TIMELINE (MET: Mission Elapsed Time)
T+ 00:00 s
Environmental Preset Configuration
ESA reference descent: 125 km entry altitude, parachute inflation at Mach 2.2, backshell jettison at 1,200 m, 4-point landing legs lock at 800 m.
Flight Dynamics Telemetry
FREQ: 10 Hz
Altitude
125.0 km
Velocity
21,000 km/h
Deceleration G
0.02 g
Dynamic Pressure
0.0 kPa
Vertical Speed
-5,833 m/s
Mach Number
Mach 27.5
ExoMars Critical Subsystems
HEALTH: NOMINAL
Ablative Front Shield
PROTECTING (540°C)
Supersonic Parachute
ARMED (M 2.2)
Backshell Separation Actuator
STANDBY (1200m)
Landing Quad-Legs Deploy/Lock
STOWED (TESTED 2024)
Terminal Pulsed Retro-Rockets
STANDBY (800m)
Manual Staging Overrides & Test Injections
EDL Mission Assessment
STATUS: READY ON ORBITAL DESCENT TRAJECTORY
Press "Execute EDL Run" or scrub the timeline to simulate atmospheric capture, parachute sequence, ESA 2024-tested backshell separation, landing leg deployment, and soft touchdown on Oxia Planum.
Press "Execute EDL Run" or scrub the timeline to simulate atmospheric capture, parachute sequence, ESA 2024-tested backshell separation, landing leg deployment, and soft touchdown on Oxia Planum.