Experimental Evaluation of High-Purity-Silica Reinforced Ablative Composites as Nozzle Sections of 7.8-Inch-/19.8 cm/ Diameter Throat Storable-Propellant Rocket Engine
1967
28 pages
Report
No indication
English
Rocket Engines & Motors , Composite Materials , Ablating material , Rocket nozzle , Silicon oxide , Storable propellant , Ablation , Char , Composite , Erosion , Evaluation , Material , Nozzle , Oxide , Propellant , Rate , Reinforced , Rocket engine , Section , Silicon , Storage