GOAL: 50% lower erosion of insulation (44% weight reduction, 7.4% booster payload increase); OBJECTIVE: Development of ceramic forming polymer and/or structurally reinforced char layer.
Solid Rocket Motor Insulation Testing
2005
16 pages
Report
Keine Angabe
Englisch
Rocket Engines & Motors , Composite Materials , Insulation , Rocket engines , Solid rocket propellants , Test and evaluation , Carbon fibers , Weight reduction , Ablative materials , Charring , Erosion resistance , Oligomers , Ceramic materials , Zirconium , Asbestos , Poss(Polyhedral oligomeric silsesquioxane) , Briefing charts
Solid rocket motor internal insulation
NTRS | 1976
|Engineering Index Backfile | 1953
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