NASA NTRS · 19930003780
Pressure fed thrust chamber technology program
Abstract
This is the final report for the Pressure Fed Technology Program. It details the design, fabrication and testing of subscale hardware which successfully characterized LOX/RP combustion for a low cost pressure fed design. The innovative modular injector design is described in detail as well as hot-fire test results which showed excellent performance. The program summary identifies critical LOX/RP design issues that have been resolved by this testing, and details the low risk development requirements for a low cost engine for future Expendable Launch Vehicles (ELVi).
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Dunn, Glenn M.. 1992-08-20. Pressure fed thrust chamber technology program. https://ntrs.nasa.gov/citations/19930003780
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