The Transient Cryogen Transfer Computer Program (TCTP) developed and verified for LOX systems by analyses of Skylab S-1B stage loading data from John F. Kennedy Space Center launches was extended to include hydrogen as the working fluid. The feasibility of incorporating TCTP into the space shuttle main engine dynamic model was studied. The program applications are documented.
Milestone report TCTP application to the SSME hydrogen system analysis
1975-12-01
Report
No indication
English
AIAA | 1989
|Report of the SSME assessment team
NTRS | 1993
Report of the SSME Assessment Team
NTIS | 1993