Abstract
The model is developed to estimate heat fluxes and temperatures at early stages of designing a system of heat-resistant coating at the critical point of the frontal bluntness of the recovery capsule without account for radiation heat flux from the air, heated behind the shock, and heat-resistant coating ablation.
Full Text 
Sign-in/Register to access full text options
Sign-in/Register to access full text options 
Paper version not known
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a call
