Military Flight Mishap Investigation & Telemetry Reconstitution Workbench

Investigation Presets F-16C Block 50 Profile

Flight Telemetry Inputs Kinetic & Aero Variables

True Airspeed (KTAS) 320 kts

Initial Altitude 15,000 ft

Flight Path Angle (γ) -12.5°

Engine Thrust 25%

Angle of Attack (α) 6.8°

Wind Shear / Crosswind 18 kts

Aviation Safety Note: Telemetry equations integrate F-16 aerodynamic polar coefficients (zero-lift drag Cd0=0.019, induced drag factor k=0.18, lift-curve slope CLa=0.075/deg) against standard ISA atmospheric lapse.

AIRCRAFT: F-16 Fighting Falcon (Single-Engine Multirole)

T+00:00 s | ISA MSL MODEL

44.3148° N, 85.6024° W (MI GRD)

Simulated Flight Path

Impact Point Vector

Glide Cone Envelope

Descent Rate 4250 feet per min (fpm)

Aerodynamic Stall Risk Moderate AoA Crit Margin: 13.2°

Glide Ratio 4.2 L/D horizontal : vertical

Impact Velocity 210 knots (indicated ground)

Reconstruction Status Simulation Verified Physics Model Converged

Export Status Ready JSON / CSV Available

Reconstituted Telemetry Time-Series Ledger

Time (s)	Alt (ft MSL)	IAS (kts)	Descent (fpm)	Pitch / FPA (°)	AoA (°)	G-Load	Phase / Status