The invention provides a step heating design method and device for simulating ballistic
ablation response and a medium, and the method comprises the steps: obtaining a
target response parameter in a flight ballistic environment, determining a
heating time length, debugging a test state, and carrying out
ablation thermal response trial calculation, and preparing an initial
simulation ablation retreat amount and a
simulation key position highest temperature for iterative calculation. Step heating state parameters of the ground
simulation test are determined through iterative calculation on the basis of the
target response parameters, and the first iteration step is used for determining the total
enthalpy coefficient of the total
enthalpy of the ground incoming flow with the matched target ablation retreat amount as the target; and the second iteration step takes the highest temperature of the matched target key position as a target and is used for determining a
heat flux density coefficient of the ground
heat flux density. According to the technical scheme, the total heating amount, the ablation amount and the highest
temperature response of the key position in the step heating state can be completely matched with the
response parameters in the flight trajectory state.