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Algorithm
Launch Lab
Dashboard
Trajectories
Heatmap
Presets
Default
Sounding
Artillery
Vacuum
Arctic
Desert
Rocket
Exhaust velocity
2500
m/s
Mass flow
50
kg/s
Initial mass
5000
kg
Fuel mass
3000
kg
Atmosphere (ISA)
Drag coefficient
0.15
Ground temp
288
K
(15°C)
Scan
Min angle °
Max angle °
Trajectories
scans
Heatmap
Y-axis
Exhaust velocity
Mass flow
Initial mass
Fuel mass
Drag coefficient
Ground temperature
Colour
Range
Altitude
Speed
Flight time
Resolution
× grid
Live — recompute as you drag
▲ LAUNCH SCAN
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ISA atmosphere · parallel Web Workers · pre-computed atlas · all in-browser ·
algorithm docs
Best Range
—
at Angle
—
Peak Alt
—
at Angle
—
Thrust
—
TWR
—
Burn
—
Source
—
←
Adjust and hit Launch
0
100
Angle
Alt (km)
Range (km)
Max v
Flight
Impact