Page
%P
![Loading...](https://link.springer.com/static/c4a417b97a76cc2980e3c25e2271af3129e08bbe/images/pdf-preview/spacer.gif)
-
Chapter and Conference Paper
Study on Matching Characteristics of Pre-cooling Air Turbo Rocket Engine
The pre-cooling air turbo rocket (PATR) engine, designed to operate with high propulsion efficiency and within a wide operating range, is one of the most promising and effective reusable single-stage in-orbit ...