COMPONENTS OF ROCKET ENGINES FOR USE IN SPACE VEHICLES-NAMELY, MULTI-PLY STRUCTURAL ABLATIVE AND INSULATIVE ROCKET NOZZLE THROAT SECTION ASSEMBLIES, CONVERGENT CONICAL SECTIONS OF ROCKET NOZZLE LININGS, DIVERGENT CONICAL SECTIONS OF EXIT CONE LININGS, EXIT CONE PRIMARY STRUCTURES, AND ROCKET NOZZLE THROAT INSERTS

'ablat':16 'assembl':23 'compon':1 'cone':36,39 'conic':25,32 'converg':24 'diverg':31 'engin':4 'exit':35,38 'insert':46 'insul':18 'line':30,37 'multi':13 'multi-pli':12 'name':11 'nozzl':20,29,44 'pli':14 'primari':40 'rocket':3,19,28,43 'section':22,26,33 'space':8 'structur':15,41 'throat':21,45 'use':6 'vehicl':10 'vehicles-nam':9

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