Abstract: The present invention provides for the integration of structural cooling and fuel treatment within hypersonic vehicles. This is achieved by channeling a hydrocarbon fuel to a portion of the aircraft structure and imparting via the heat sink effect sufficient heat to cause a pyrolysis of the hydrocarbon fuel. After pyrolysis, the resulting fractions are then utilized as a fuel by the vehicle.
Type:
Grant
Filed:
January 30, 1992
Date of Patent:
August 17, 1993
Assignee:
Rockwell International Corporation
Inventors:
Herbert R. Lander, Robert E. Schnurstein