minor progress report.....
well, this wednesday was a national holliday, so i got myself a couple of rather insufficient hours of able time on the '42 project....
it was enough to pull off a thing or two tho.... but unfortunately most of it was just intangible research work - with the exception of the now-animated tiller handle for the nosewheel steering (only when on ground) plus a couple of tuneups for the flight model....
but more impotantly, i've learned a few new things about ram/scramjet design - and might be worth it to redo some code for a much more realistic representation of how a thing like that would work... (and here we go on the "how to build the thing for real" discussion again)
the first key concept - the need for a mighty turbopump
an engine like that doesn't light itself up - fuel must be pumped to something like 100bar for injection.... that requires a big beefy pump, a heavy pump....
but - having more engines aboard, two additional options came to mind to remove that extra weight
* we can use a crossfeed system and use the two main engines to pump fuel for the ramcaster - would require oxidizer flow, tho.... could be less than optimal in terms of efficiency
or.....
* we can rev up the APU and use that to drive this pump - it already runs on monopropellant, so no oxidizer would be needed (it would need to burn from the RCS//OMS supply during ramcaster ascent, tho)
i find the second solution to be generally more agreeable (and less heavy on redesign work than the first one...) - so i just might go with that...
now, the second thing.... this is more complex stuff
the constant dynamic pressure flightpath
up to now, the optmal ascent path was defined somewhat arbitrarily through a lookup bitmap reference interpolation process....
but having a better understanding of how real scramjets perform, i feel there could be a LOT of room for improvement on that whole area
i don't plan on removing the lookup table scheme altogether - but i just might have it redone over different parameters... so instead of a mach x altitude table as it's been so far, we'd have a dynamic pressure x mach reference lookup, providing a far more accurate representation of what a ramcaster ascent would be like if it were for real
needless to say, this is kinda bad news for that flight manual.... for if i'm gonna change stuff around, writing about it is just south of conterproductive, i suppose :hmm:
so please be patient.... there shall be a manual, as soon as there's something less, ehmm... "variable" to write about :lol: - in the meantime, help eachother out as you can, and don't hesitate to ask me about anything (even if it seems too obvious)
i guess i shall update to WIP-303 with the current state as is.... these new changes are meaningful enough to qualify as WIP-4
well.... back to work