Method and apparatus for pressure pulse arcjet starting
AssigneeThe United States of America as represented by the Administrator of the National Aeronautics and Space Administration
InventorsJohn M. Sankovic, Francis M. Curran
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Abstract
The invention disclosed is directed to a method and apparatus for an arcjet starter. The invention discloses a method of moving an arc from the subsonic region of the thruster to the supersonic region by introducing a pressurized propellant into the casuty of the anode.
Claims3
A method of arcjet starting, said arcjet starter including a power processing unit, a propellant source, a first valve serially connected to said propellant source, a first gas generator serially connected to said first valve, a second valve serially connected to said propellant source, a second gas generator serially connected to said second valve and arcjet thruster serially connected to said first and second valve, wherein said second valve and said second gas generator are arranged in parallel with said first valve and said first gas generator, said method comprising the steps of:
- simultaneously opening said first valve and closing said second valve whereby propellant flows from said propellant source through said gas generator to said arcjet thruster thereby creating a first pressure in said arcjet thruster,
- cycling said second valve open and close whereby a pressure pulse is created thereby producing a second pressure in said arcjet thruster,
- utilizing said power processing unit to initiate high voltage pulses in said arcjet thruster as said second pressure monotonically decreases to said first pressure thereby starting said arcjet thruster.
An apparatus for pressure pulse arcjet starter, comprising:
- a propellant source for delivering propellant flow to an arcjet thruster,
- a first valve serially connected to said propellant source for controlling propellant flow between said propellant source and said arcjet thruster,
- a first gas generator positioned between said first valve and said arcjet thruster for processing said propellant flow,
- a second valve serially connected to said propellant source and parallel to said first valve for cyclically controlling said propellant flow,
- a second gas generator serially connected to said second valve and parallel to said first gas generator for processing said cyclically controlled propellant flow thereby providing redundancy for said apparatus for pressure pulse arcjet starting.
Dependencies are inferred from the claim text.