KSP MEM (Munar Module) Ascent Stage Test

[Pawelk198604]

Recently i found really cool stuff monopropellant engines, i think it really cool to use it in my design of ascent of my laander, i'm also couscous how looked the real ascent stage of Apollo landers?

Now I just have to figure out how to fit the lander, beneath the.command module, plan to use this super huge boosters form NASA.

I would glad for you feedback.

[Volcanix]

Mhh.. I'm sorry, do you want feedback on your current rocket or do you want help on building the lander ?

I'm not quite sure but well I am quite sure that the Saturn V was the launch vehicle for the apollo missions.

I think this is the information and pictures you wanted.

Let me know what you meant.

Edited August 27, 2014 by Volcanix
typo.. is it called like this? :I

[Horn Brain]

Saturn V, not Falcon. Falcon is SpaceX stuff.

The LM looks like this:

It used hypergolic fuels, not monopropellant, and had two engines, both in the center of the vehicle. You can see the ascent engine is recessed into the cabin area.

If I were you, I would cut way back on fuel for both stages. You only need about 700 m/s max to land on the Mun from LMO, and that's granting a generous saftey margin. Likewise, you need the same dv to get back up.

[Volcanix]

Saturn V, not Falcon. Falcon is SpaceX stuff.

Oh yeah, sorry. Of course I meant the Saturn V. Thought of SpaceX during writing it.. xd just gonna edit it^^