Flight Parameters
STAGE 1
Engine Thrust
110 kN
Launch Angle (Tilt)
88°
Burn Duration
145 s
Payload Mass
2,400 kg
Drag Coefficient (Cd)
0.30
Target Apogee Ref
105 km
Peak Altitude (Apogee)
106.4 km
✓ Karman Line Crossed
Microgravity Time
218 s
Weightless Arc (>80km)
Peak Re-Entry Decel
5.2 G
Nominal Braking
Re-Entry Velocity
1,120 m/s
Max-Q: Dynamic Drag
Flight Telemetry Analysis & Export
Profile loaded: Suborbital Tourism preset. Peak apogee reaches 106.4 km, penetrating past the 100 km Karman line into low-density thermosphere space. Spacecraft passengers experience ~218 seconds of continuous weightlessness before atmospheric braking yields a peak G-force deceleration load of 5.2 G.