NASA NTRS · 19720016184
Development of low cost fabrication techniques for large solid rocket nozzles
Abstract
Property measurements and fabrication characteristics were determined and the performance in subscale (Minuteman Wing 2 second stage) motors was evaluated. It was demonstrated that the incorporation of low cost fabrication techniques in a full scale 260 in. nozzle could result in savings of $149,000 when compared with an identical design using tape-wrapped components throughout.
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Warga, J. J.. 1971-09-01. Development of low cost fabrication techniques for large solid rocket nozzles. https://ntrs.nasa.gov/citations/19720016184
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