Resources Contact Us Home
Structure and method for controlling inlet shock position of a hypersonic vehicle

Image Number 2 for United States Patent #6880342.

System and method for controlling inlet shock position and airflow Mach number of a hypersonic vehicle is described wherein thermally controlled fuel is controllably injected into the airflow at the inlet of the propulsion system of the vehicle.

  Recently Added Patents
Image-processing method and program, and image-processing apparatus
Compounds, compositions and use
Anti-slip strip for vehicle running boards
Biaxially oriented film which could be thermally laminated with paper and other substrates
Audio conversation apparatus
System and method for optimizing utilization of inventory space for dispensable articles
Method for the hydrolysis of substituted formylamines into substituted amines
  Randomly Featured Patents
Magnetically levitated apparatus
Seal rupture mechanism for a gas source
Sound-picture synchronous compression and synchronous reproduction system
Driver circuit for a D.C. motor without commutator
Orifice restriction shielding device
Method of identifying information addressed to a user in a communication system and a communication system
Integrated filter in antenna-based detector
Lathe compound multi-tool
Contractible handcuff
High purity 2,4-dinitrotoluene from toluene nitration process