Apparatus for staged combustion in air augmented rockets
AssigneeThe United States of America as represented by the Secretary of the Army
InventorRichard G. Rhoades
Life of this patent
Estimating the term…
Abstract
Apparatus for providing staged addition of air to the ramburner of an air gmented rocket for enhancing the ignition, combustion, and performance of the rocket. A shaped, strut-mounted, ablative-coated sleeve is mounted coaxially in the ramburner section of the rocket. This sleeve causes the diversion of a part of the inlet air and provides a favorable regime for ignition and combustion of the air augmented propellant. The diverted air is subsequently added to the combustion region through passageways in the sleeve. The shaped combustible ablative material of the sleeve provides additional thrust-producing fuel to the ramburner.
Claims2
Apparatus for providing staged addition of air to the ramburner of an air augmented rocket comprising:
- a. a ramburner including a combustion region, said ramburner having a forward portion provided with air inlets and an aft portion provided with a nozzle;
- b. an air staging device disposed intermediate said air inlets and said nozzle, said staging device disposed for metering air flow to said combustion chamber for enhancing the ignition combustion and performance of said rocket, said air staging device being a tapered cylindrical member having apertures disposed in radial and longitudinal spaced relation in the surface thereof for directing a portion of said air to said combustion chamber, said staging device further having a coating of ablative material thereon for providing additional thrust producing fuel to the ramburner as well as providing thermal protection;
- and,
- c. A mixing chamber disposed intermediate said nozzle and said cylindrical member to receive air passing around said staging device for mixing with the combustion products issued from said combustion region.
Dependencies are inferred from the claim text.