Download or read book Asrm Nozzle Thermal Analysis written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-17 with total page 102 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report describes results from the nozzle thermal analysis contract which has been performed to support NASA/Marshall Space Flight Center in the development of the Advanced Solid Rocket Motor (ASRM). The emphasis of this study has been directed to four potential problem areas of the nozzle. These areas are the submerged nozzle region containing the flex seal, the nozzle entrance region, the material interface region in the nozzle exit cone, and the aft region of the exit cone. This study was limited throughout by inadequate material response models, especially for the polyisoprene flex seal and the low density carbon phenolic used in the exit cone. Thermal response and particle erosion calculations were performed for each of the potential problem areas. Results from these studies showed excessive erosion (large negative safety margins) to occur in the flex seal and nozzle entrance regions. The exit cone was found to be marginally adequate (near zero safety margins) and the material interface region was found not to be a problem. Strobel, Forrest and King, Belinda Unspecified Center ADVANCED SOLID ROCKET MOTOR (STS); EROSION; FLOW DISTRIBUTION; ROCKET NOZZLES; SAFETY FACTORS; SEALS (STOPPERS); THERMAL ANALYSIS; CARBON-PHENOLIC COMPOSITES; CONVECTIVE HEAT TRANSFER; POLYISOPRENES; TEMPERATURE EFFECTS; THERMOCHEMICAL PROPERTIES; THERMOCHEMISTRY...
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Download or read book NASA Reports Required by Congress written by United States. Congress. House. Committee on Science, Space, and Technology. Subcommittee on Space Science and Applications and published by . This book was released on 1992 with total page 894 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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Download or read book An Analysis of Thermal Radiation Heat Transfer in a Nuclear rocket Nozzle written by William H. Robbins and published by . This book was released on 1961 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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