T
thereiwas
Guest
Ok, 8t mass, 20m ballute, slows to 94.4 m/s at 137m. But we are talking over 500 kN of thrust to stop it. Raising engine start to 300m requires a peak thrust of more like 240 kN, but consumes nearly twice as much fuel (assuming fuel consumption is linear with thrust level).<br /><br />For comparison the SM engine on Apollo only put out 92 kN of thrust. May need solids anyway for main braking impetus. I am looking at a touchdown speed of 1.4 m/s.<br /><br />Some details: at 300m descending at 94.4m/s, you have just over 3 seconds to stop. To slow from 94.4m/s in 3 seconds is 30 m/s/s. (3 G's; I don't think we want to go higher.) Imparting 30 m/s/s to 8t needs (F=ma) 240 kN, unless I am making some simple mistake in the equations.