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 the condenser is connected to {TAIL ~ at least one combustion system} of the airplane engine 
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 the condenser is connected to { TAIL ~ 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 OTH OTH OTH REL REL REL TAIL TAIL TAIL TAIL TAIL TAIL TAIL TAIL TAIL OTH OTH OTH OTH