Thermal Profiles of the delta Spacecraft Fairings Heos-A2 Thermal Profile, Volume 7

摘要

The HEOS-A2 mission will utilize the DSV-3L launch vehicle. A profile of the DSV-3E-7 fairing, showing several points of analysis, is presented. The predicted inner wall temperature histories of the HEOS-A2 fairing are based on a depressed trajectory and the corresponding angle of attack history. (Author)