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- W2081067821 abstract "In this paper∗ two observations are made in the context of lifting re-entry. One is that, during re-entry itself, much higher lift coefficients (both at maximum lift and per unit lift-drag ratio) can be provided by variants of the caret wing than by flat-bottomed delta wings or other vehicles that give high spillage. The second is that, after re-entry and whether vehicles are flat-bottomed or recessed, they can glide hypersonically at much higher lift-drag ratios than are commonly assumed. These features are additional to that of aerodynamic simplicity, on which the caret wing was originally advocated by Nonweiler. Both would be desirable for Space Shuttle orbiters: the first because, for a given wing loading, it will moderate re-entry heating rates and/or increase re-entry range: and the second, because it improves cross-range during the subsequent glide by many hundreds of miles, and thereby the operational flexibility which is a primary requirement for Space Shuttle systems." @default.
- W2081067821 created "2016-06-24" @default.
- W2081067821 creator A5071649672 @default.
- W2081067821 date "1972-01-01" @default.
- W2081067821 modified "2023-09-25" @default.
- W2081067821 title "Some design aspects of space shuttle orbiters" @default.
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- W2081067821 doi "https://doi.org/10.1016/0376-0421(72)90015-2" @default.
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