- Restrictions on Access:
- Unclassified, Unlimited, Publicly available.
- The efforts to adapt CHAM's computational fluid dynamics code, PHOENICS, to the analysis of flow within the high pressure fuel turbopump (HPFTP) aft-platform seal cavity of the SSME are summarized. In particular, the special purpose PHOENICS satellite and ground station specifically formulated for this application are listed and described, and the preliminary results of the first part two-dimensional analyses are presented and discussed. Planned three-dimensional analyses are also briefly outlined. To further understand the mixing and combustion processes in the SSME fuelside preburners, a single oxygen-hydrogen jet element was investigated.
- NASA Technical Reports Server (NTRS) Collection.
- Document ID: 19850006553.
Accession ID: 85N14862.
- No Copyright.
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