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- W2077910212 abstract "This paper presents an analysis of data obtained from wind tunnel tests of the aerodynamic interference induced by the reaction control system jets on Space Shuttle orbiter configurations. The test data was obtained using cold gas simulation techniques with nozzles scaled to match jet exit momentum ratio as the primary parameter at Mach numbers from 2.5 to 10. Significant induced effects have been found that degrade the performance of the pitch and roll reaction controls and that induce cross-coupling effects for yaw reaction control. Analysis of the induced data shows good correlation with jet exit momentum ratio." @default.
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- W2077910212 date "1974-08-16" @default.
- W2077910212 modified "2023-09-23" @default.
- W2077910212 title "Reaction control system plume flow field interaction effects on the Space Shuttle orbiter" @default.
- W2077910212 doi "https://doi.org/10.2514/6.1974-1104" @default.
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