NASA NTRS · 19810006504
Orbit transfer vehicle advanced expander cycle engine point design study. Volume 2: Study results
Abstract
The design characteristics of the baseline engine configuration of the advanced expander cycle engine are described. Several aspects of engine optimization are considered which directly impact the design of the baseline thrust chamber. Four major areas of the power cycle optimization are emphasized: main turbine arrangement; cycle engine source; high pressure pump design; and boost pump drive.
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Diem, H. G.. 1980-12-12. Orbit transfer vehicle advanced expander cycle engine point design study. Volume 2: Study results. https://ntrs.nasa.gov/citations/19810006504
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