Computer Science – Performance
Scientific paper
Dec 1992
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1992asee.nasar....f&link_type=abstract
In Alabama Univ., 1992 NASA/ASEE Summer Faculty Fellowship Program 5 p (SEE N93-17279 05-80)
Computer Science
Performance
Hybrid Propulsion, Liquid Oxidizers, Propulsion System Configurations, Propulsion System Performance, Cargo, Ducted Rocket Engines, Launch Vehicles, Performance Prediction, Solid Fuels, Titan
Scientific paper
A hybrid rocket is a system consisting of a solid fuel grain and a gaseous or liquid oxidizer. Figure 1 shows three popular hybrid propulsion cycles that are under current consideration. NASA MSFC has teamed with industry to test two hybrid propulsion systems that will allow scaling to motors of potential interest for Titan and Atlas systems, as well as encompassing the range of interest for SEI lunar ascent stages and National Launch System Cargo Transfer Vehicle (NLS CTV) and NLS deorbit systems. Hybrid systems also offer advantages as moderate-cost, environmentally acceptable propulsion system. The objective of this work was to recommend a performance prediction methodology for hybrid rocket motors. The scope included completion of: a literature review, a general methodology, and a simplified performance model.
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