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