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LOW-COST FABRICATION TECHNIQUES FOR SOLID ROCKET NOZZLES
ISSN: 0148-7191, e-ISSN: 2688-3627
Published February 01, 1970 by SAE International in United States
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Savings of 50 percent can be achieved in ablative nozzles for 260-in.-dia solid rocket motors using present state-of-the-art materials. An optimum nozzle design with respect to cost and performance results from the use of a standard carbon-phenolic tape grade for the throat insert and canvas, carbon-silica and silica materials throughout the remainder of the nozzle.
CitationWARGA, J., "LOW-COST FABRICATION TECHNIQUES FOR SOLID ROCKET NOZZLES," SAE Technical Paper 700796, 1970, https://doi.org/10.4271/700796.
- Warga, J. J. et al. Evaluation of Low-Cost Materials and Manufacturing Processes for Large Solid Rocket Nozzles December 1967 This has been excerpted and published in the Science of Advanced Materials and Process Engineering Series 15 435 444 1969
- Mathis, J. R. Larrabee C. R. Development of Low-Cost Ablative Nozzles for Solid Propellant Rocket Motors February 1970
- Warga, J. J. Investigation of Effects of Ablative Discrepancies on Nozzle Performance Reliability May 1970
- Lampman, J. J. Warga J. J. Davis H. O. Deviation Nozzle Program June 1968
- King, C. B. Dielectric Processing for Low-Cost Ablation Heat Shields Science of Advanced Materials and Process Engineering Series 15 445 453
- Savage, E. E. Optimization of 260-in. Diameter Motor with Low-Cost Materials June 1970