A propellant tank is connected to the in flow side of the condenser and stores the cryogenically stored propellant, wherein {HEAD ~ the out flow side} of {TAIL ~ the condenser} is connected to at least one combustion system of the airplane engine 
of
A propellant tank is connected to the in flow side of the condenser and stores the cryogenically stored propellant , wherein { HEAD ~ the out flow side } of { TAIL ~ the condenser } is connected to at least one combustion system of the airplane engine
OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH HEAD HEAD HEAD HEAD HEAD HEAD HEAD HEAD REL TAIL TAIL TAIL TAIL TAIL TAIL OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH