This presentation discusses the work towards a second generation
reusable launch vehicle (RLV). The goals of the second generation
RLV program are reviewed. These include cost, safety, and
propulsion advances. The Fluid dynamics technologies under
development are discussed. These include the altitude compensating
nozzle technology, the Aerospike plume induced base heating, the
inducer testing technology. Pictures of altitude compensating
nozzles Aerospike Plume Induced Base Heating results and Inducer
testing technologies are included. Further goals of the program are
to improve the methodology for optimizing design of the injectors,
to improve the optimization of the turbopump and improvement of the
methodology to analyze the engine performance. This presentation
consists of outline view slides.
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