Lunar Return Aerobrake

110 km perigee · Raptor vac Isp 380 s · belly-flop attitude

Inputs

100 t
10900 m/s
20 t
40 m/s
400 km
2.0 m/s

Outputs

Capture Δv
—
Perigee vel.
—
Initial apogee
—
First period
—
Passes
—
Total time
—
Peak heat flux
—
Heat / pass
—
Peak tile temp
—
Peak g-load
—
Total heat
—

Propellant budget

Capture burn
—
RCS (all passes)
—
Final raise Δv
—
Final raise prop.
—
Total used
—
Margin
—
Day0.00
Pass0
Apogee— km
Velocity— km/s
1.0 days/s

Apogee altitude (log)

Mission time vs propellant