This paper presents results from arc jet tests conducted at the NASA Johnson Space Center on reinforced carbon-carbon (RCC) samples subjected to hypervelocity impact. The RCC test specimens are representative of RCC components used on the Space Shuttle Orbiter. The arc jet testing established the oxidation characteristics of RCC when hypervelocity projectiles, simulating meteoroid/orbital debris, impact the RCC material. In addition to developing correlations for use in trajectory simulations, we discuss analytical modeling of the increased material oxidation in the impacted area using measured hole growth data. Entry flight simulations are useful in assessing the increased Space Shuttle RCC component degradation as a result of impact damage and the hot gas flow through an enlarging hole into the wing leading-edge cavity.Curry, Donald M. and Pham, Vuong T. and Norman, Ignacio and Chao, Dennis C.Johnson Space CenterCARBON-CARBON COMPOSITES; HYPERVELOCITY IMPACT; OXIDATION; ARC JET ENGINES; HYPERVELOCITY PROJECTILES; IMPACT TESTS; SPACE DEBRIS; TEST FACILITIES; MATHEMATICAL MODELS; FLIGHT SIMULATION...