Trajectory & Alpine Terrain Profile (HUD Cross-Section)
PHASE: STABILIZED DESCENT
[0.00s] Canopy Jettison command initiated by lower ejection handle pull.
[0.35s] Martin-Baker SJU-17 catapult fire. Seat rails cleared.
[0.55s] Rocket sustainers ignite (18G max acceleration).
[1.10s] Drogue chute deployment for aerodynamic seat stabilization.
[1.65s] Seat separation sequencer releases harness straps.
[2.40s] Main parachute full canopy inflation at safe terrain clearance.
Entry Parameters & Mountain Atmospheric
ENVELOPE SAFE
Search & Rescue (SAR) Telemetry & Beacon Envelope
| Pilot Apogee Altitude: | 8340 ft MSL |
| Seat Separation Time: | 1.65 s |
| Full Canopy Altitude: | 7720 ft MSL |
| Terrain Clearance Margin: | 4120 ft |
| Canopy Wind Drift: | 0.84 NM |
| Total Descent Time: | 168.4 s |
| Impact vs Touchdown Separation: | 1420 m |
| SAR Primary Search Radius: | 680 m |