awesome plane, Nutty! :thumbup: - kudos on your aero-modeling skills!
and you win one free internet for pointing out the rudder dynamics - i had not thought of that!
the reason why the G42's "rudderbrakes" have very little effect on direction, is that they are currently implemented as actual "rudders" as far as orbiter is concerned :hmm:... and without a meaningful vertical surface area, although rotation is applied, very little lateral acceleration takes place... this is because Orbiter is mostly unaware of the drag being caused by the rudderbrakes
now, by seeing how your plane flies, i'll have to try something different - i shall REMOVE the code for rudders, and replace it by independent "variable-drag" elements (aka: Airbrakes), to be controlled by the rudder axis
doing it this way should "force" Orbiter to simulate the true effects of this type of rudder - i hope
i'm not sure how it's gonna behave, but it should indeed have a little more effect on direction, i guess...
remember, an empty G42 weighs 38 tons, and flies at about 500km/h... i don't know how much effect the rudderbraks should have, in comparison to your awesome little plane... i guess we shall soon find out :hmm:
---------- Post added 09-21-10 at 10:52 AM ---------- Previous post was 09-20-10 at 11:18 AM ----------
i was thinking today....
the G42 needs to haul 30 tonnes of LOX about half-way up to orbit so it can have something to burn on the main engines in the last stage....
but - what if - instead of a full LOX tank, the G42 could takeoff with an EMPTY one and a ram-stream compressor?
it hit me that we could save 30 tons of takeoff mass by developing some form of collecting the needed oxidizer "on the fly" - when the LOX tanks become full, over half the propellant would have already been used :hmm:
but there are a few hindrances one must overcome to make this viable....
namely, the heat --
at mach 14, at which point the collector scoop/probe/thingy would open, the incoming air is insanely hot... now, i reckon most gasses take up an awful lot of volume when in high temperature.... this could be a problem, being that we're trying to compress such gas
it would need cooling - and LOTS of it...
now, the G42 burns dense fuels, which are stored at mostly mundane temperatures (unlike LH2, which is tanked at cryogenic levels)... with that, we can't really use our own fuel to cool off the incoming air, as the SABRE engines would do....
30 tonnes is still a nice mass relief, but i wonder what amounts of coolant would be needed by this system
so, once again, i beckon all the OF sim-scientists to pitch in with ideas on how this could work
30 tons of takeoff mass - that's almost as much as the empty mass of the whole ship...
and you win one free internet for pointing out the rudder dynamics - i had not thought of that!
the reason why the G42's "rudderbrakes" have very little effect on direction, is that they are currently implemented as actual "rudders" as far as orbiter is concerned :hmm:... and without a meaningful vertical surface area, although rotation is applied, very little lateral acceleration takes place... this is because Orbiter is mostly unaware of the drag being caused by the rudderbrakes
now, by seeing how your plane flies, i'll have to try something different - i shall REMOVE the code for rudders, and replace it by independent "variable-drag" elements (aka: Airbrakes), to be controlled by the rudder axis
doing it this way should "force" Orbiter to simulate the true effects of this type of rudder - i hope
i'm not sure how it's gonna behave, but it should indeed have a little more effect on direction, i guess...
remember, an empty G42 weighs 38 tons, and flies at about 500km/h... i don't know how much effect the rudderbraks should have, in comparison to your awesome little plane... i guess we shall soon find out :hmm:
---------- Post added 09-21-10 at 10:52 AM ---------- Previous post was 09-20-10 at 11:18 AM ----------
i was thinking today....
the G42 needs to haul 30 tonnes of LOX about half-way up to orbit so it can have something to burn on the main engines in the last stage....
but - what if - instead of a full LOX tank, the G42 could takeoff with an EMPTY one and a ram-stream compressor?
it hit me that we could save 30 tons of takeoff mass by developing some form of collecting the needed oxidizer "on the fly" - when the LOX tanks become full, over half the propellant would have already been used :hmm:
but there are a few hindrances one must overcome to make this viable....
namely, the heat --
at mach 14, at which point the collector scoop/probe/thingy would open, the incoming air is insanely hot... now, i reckon most gasses take up an awful lot of volume when in high temperature.... this could be a problem, being that we're trying to compress such gas
it would need cooling - and LOTS of it...
now, the G42 burns dense fuels, which are stored at mostly mundane temperatures (unlike LH2, which is tanked at cryogenic levels)... with that, we can't really use our own fuel to cool off the incoming air, as the SABRE engines would do....
30 tonnes is still a nice mass relief, but i wonder what amounts of coolant would be needed by this system
so, once again, i beckon all the OF sim-scientists to pitch in with ideas on how this could work
30 tons of takeoff mass - that's almost as much as the empty mass of the whole ship...