F-16 Flight Emergency & ACES II Ejection Envelope Simulator

Based on Yalova Training Incident Physics • Aerodynamic Glide & ACES II Ejection Dynamics

PRESETS:
IAS: 280 KTS
ALT: 4500 FT AGL
SINK: -2400 FPM
PITCH: 2.5°
G-FORCE: 1.0 G
STATUS: IN GLIDE

COCKPIT FLIGHT TRIM & EMERGENCY COMMANDS

MODE: ACES II MANUAL OVERRIDE
2.5°
Nose Down (-10°) Optimal Glide Nose Up (+15°)
AIRBRAKES / DRAG:

Deploying airbrakes trades airspeed for a steeper descent gradient prior to ejection.

EMERGENCY PROCEDURE: PULL EJECTION HANDLE WHEN BELOW SAFE ENVELOPE MARGINS

ACES II SAFE EJECTION ENVELOPE

AIRSPEED VS ALTITUDE
Safe Corridor Unrecoverable/Fatal Current Aircraft State

LIVE FLIGHT TELEMETRY DATA

CURRENT ALTITUDE 4500 FT
AIRSPEED (IAS) 280 KTS
VERTICAL SPEED -2400 FPM
GLIDE RATIO (L/D) 8.2 : 1
TIME TO TERRAIN 112.5 SEC
MIN SAFE EJECT ALT 800 FT

FLIGHT DYNAMICS LOG & ACES II SEQUENCE REPORT

Timestamped record of flight glide decay, pilot rocket ejection, drogue chute stabilization, and ground touchdown metrics.

TIME (S) ALTITUDE (FT) AIRSPEED (KTS) SINK RATE (FPM) PITCH (°) SEQUENCE STAGE ENVELOPE STATUS
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