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.
Development of low cost fabrication techniques for large solid rocket nozzles
1971-09-01
Report
No indication
English
Low-Cost Fabrication Techniques for Solid Rocket Nozzles
NTIS | 1970
|LOW-COST FABRICATION TECHNIQUES FOR SOLID ROCKET NOZZLES
SAE Technical Papers | 1970
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