The combustion system for the Advance Expander Test Bed engine consists of a thrust mount, an injector with a H2-O2 torch igniter, a combustion chamber, and a conical nozzle extension. These components constitute the thrust chamber assembly. The design, fabrication, and testing of these components are described in detail.
Design and fabrication of a hydrogen/oxygen thrust chamber assembly
AIAA, SAE, ASME, and ASEE, Joint Propulsion Conference and Exhibit ; 1993 ; Monterey, CA, United States
1993-06-01
Conference paper
No indication
English
Springer Verlag | 2020
|