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Method of manufacturing a rocket combustion chamber

  • US 4,508,680 A
  • Filed: 06/01/1983
  • Issued: 04/02/1985
  • Est. Priority Date: 06/08/1982
  • Status: Expired due to Fees
First Claim
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1. A method for manufacturing the cooling wall of a rocket combustion chamber, comprising the steps of:

  • making an inner cylinder of a metallic material formed with grooves in the exterior surface thereof;

    filling up the grooves of said inner cylinder with a filler;

    compression-molding an outer cylinder on the inner cylinder by uniformly compressing metallic material powder of a predetermined thickness against the entire outermost surface of the inner cylinder having its grooves filled up with the filler;

    removing the filler from the grooves of said inner cylinder, whereby the grooves remain as empty cooling channels; and

    sintering the compression-molded powder to join the sintered outer cylinder material to the inner cylinder material and to form integral inner and outer cylinders with cooling channels therebetween.

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