Abstract
The mechanical structure and thermal system of the OBC was designed by the IRS. With this approach it was possible to find a configuration of the OBC housing and electronics as compact as possible and well adapted to the FLP target spacecraft.
Author supplied keywords
Cite
CITATION STYLE
APA
Lengowski, M., & Steinmetz, F. (2013). OBC Mechanical and Thermal Design. In Springer Aerospace Technology (pp. 133–150). Springer Nature. https://doi.org/10.1007/978-3-642-35557-8_7
Register to see more suggestions
Mendeley helps you to discover research relevant for your work.
Already have an account? Sign in
Sign up for free