Rocket Physics Failure Simulator

Stage Specifications

TWR: 1.72

FLIGHT CONFIGURATION PRESETS

Sea-Level Thrust 7,500 kN

Propellant Mass 420,000 kg

Dry Structural Mass 25,000 kg

Specific Impulse (Isp) 311 s

Structural Safety Margin 1.15x (Thin-Walled)

Physics Constraints: Max-Q occurs when air density × velocity squared peaks. If aerodynamic stress exceeds the fuselage limit (40.0 kPa), catastrophic structural failure occurs immediately.

Altitude

0.0km

Velocity

0.0m/s

Dynamic Q

0.0kPa

Propellant

100%

100km 75km 50km 25km 0km

MAX-Q LOAD 0%

STANDBY - READY FOR TEST

Awaiting ignition. Configured for high-thrust ascent through thick lower atmosphere. Click IGNITE & LAUNCH to verify if the fuselage withstands aerodynamic shearing.

Metric	Flight Peak	Threshold / Nominal	Assessment
Max Velocity	0.0 m/s	≥ 7,800 m/s	Sub-orbital
Peak Dynamic Pressure (Max-Q)	0.0 kPa	40.0 kPa	Nominal
Apoapsis (Max Altitude)	0.0 km	≥ 160.0 km	Ground