Structural G-Load

ACCELERATION STRESS PROFILE

MISSION ACCELERATION TIMELINE PRESET

TOTAL ENGINE THRUST (NEWTONS)

TOTAL VEHICLE MASS (m- KILOGRAMS)

ATMOSPHERIC DRAG FORCE (D - NEWTONS)

MATRIX LIVE

G-LOAD ANALYZER

Drag/Touch to Rotate Structural Load Planes

TOTAL COMBINED LOAD FACTOR

0.00

G-FORCE ACCELERATION UNITS

STRUCTURAL STABILITY & HUMAN LIMIT SPECS:

AWAITING IGNITION VECTOR

Net Vehicle Linear Acceleration ($a$)0.00 m/s²

Thrust-to-Weight Ratio ($TWR$)0.00

NEW HORIZONS MISSION CONTROL • TELEMETRY FLIGHT DYNAMICS SYSTEM 2026

Vector G-Load

Apparent Weight. G-load is the Stress Factor. It measures the force exerted on the structure of a rocket—and the body of the pilot—during intense acceleration.

🏎️ Linear: Felt during rapid takeoff or braking.
🔄 Centripetal: Felt during sharp high-speed turns.
🥨 Structural: High Gs can snap wings or crush fuel tanks.

👨‍🚀

⚠️ HIGH G-LOAD

BIOMETRIC SCAN

8.4 G

STATUS: 🚨 CRITICAL TOLERANCE

INERTIA-SYNC ACTIVE ✅

Radius R

The Geometry of Speed. Turn Radius is the Tension of the Arc. If you double your speed, you need four times the radius to keep the same G-load.

🏁 Small Radius: High G-load, sharp maneuver.
🌍 Large Radius: Smooth curve, lower stress.
🛰️ Orbit: A permanent turn around a planet.

🛰️

Vector Analysis

R: 450m

📐 STEADY STATE

RADIUS-SYNC ACTIVE ✅

Dry Mass Md

The Empty State. Dry Mass is the Structural Limit. It is the weight that doesn't disappear during flight, acting as the ultimate tax on your engine's efficiency.