Orbital Ascension Simulator

From Duluth to LEO: A Solid-Propellant Trajectory Model
PHASE: PRE-LIGHT

Vehicle State

ALTITUDE0.0 km
VELOCITY0.0 m/s
MASS0.0 kg
G-LOAD0.0 g

Atmospheric Profile

DENSITY1.225 kg/m³
TEMP15.0 °C
PRESSURE101.3 kPa
DRAG COEF0.00

Engine Telemetry

THRUST0.0 kN
ISP0 s
FLOW RATE0.0 kg/s
TIME ELAPSED00:00