21st AIAA International Space Planes and Hypersonics Technologies Conference 2017
DOI: 10.2514/6.2017-2173
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Aerodynamic configuration design and optimization for hypersonic vehicles

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Cited by 3 publications
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“…It has a conical design and an estimated L/D of about 2.2-lower than that of the HTV-2, which had L/D of 2.6. 33 As a result, the DoD's decision to pursue a more mature technology will likely result in a BGV with less range and maneuverability than a successful wedge design with higher L/D would have. 34 This also means that the computational model we developed in Paper 1, based on the wedge design of the HTV-2, may somewhat over-estimate the flight performance of the C-HGB.…”
Section: Evolution Of the Us Hypersonic Programmentioning
confidence: 99%
“…It has a conical design and an estimated L/D of about 2.2-lower than that of the HTV-2, which had L/D of 2.6. 33 As a result, the DoD's decision to pursue a more mature technology will likely result in a BGV with less range and maneuverability than a successful wedge design with higher L/D would have. 34 This also means that the computational model we developed in Paper 1, based on the wedge design of the HTV-2, may somewhat over-estimate the flight performance of the C-HGB.…”
Section: Evolution Of the Us Hypersonic Programmentioning
confidence: 99%