jim beam
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Gas Generator Cycle for Rocket Engines - Variants
in Engineering
Posted · Edited by jim beam
sorry for my bad english
and this is properly not the right thread for this type of question
i thinking about a alternative for a rocket turbo pump motor (just thinking)
i shoud be easy to construct, reliable and "cheap"
i ended with a combustion engine fed with compressed air (nitrogen/ oxygen mixture) and gasoline of corse
sounds stupid, but i think i coud work.
a very simplified calculation:
e.g. a 1l 4-stroke engine engine shoud breathes @ 10k rpm 5000l air per minute, burning duration 240sec -> 10000l
air can easy compressed to 300bar (as far as i know) -> a ~34l pressure bottle (and small amount of gasoline) should be enough for 240 sec run-time.
for performance tuning of the combustion engine the use of slightly more oxgen in mixture than normal air shoud work to (until the motor burns )
advantage:
- relatively lightweight
- reliable
- easy to constuct (modification of existing motors)
- easy throttling and restating
- relatively high efficiency ?!
complete nonsense or something that might work ? (e.g. for projects like http://copenhagensuborbitals.com)
some (usefull) respond would be nice!
best regards