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A sizing-based approach to evaluate hypersonic demonstrators: demonstrator-carrier constraints

Published online by Cambridge University Press:  17 April 2020

J.G. Haley Open the ORCID record for J.G. Haley [Opens in a new window] ,
T.P. McCall Open the ORCID record for T.P. McCall [Opens in a new window] ,
I.W. Maynard Open the ORCID record for I.W. Maynard [Opens in a new window]  and
B. Chudoba
J.G. Haley*
Affiliation:
The University of Texas at Arlington, Arlington, TX76019, USA
T.P. McCall
Affiliation:
The University of Texas at Arlington, Arlington, TX76019, USA
I.W. Maynard
Affiliation:
The University of Texas at Arlington, Arlington, TX76019, USA
B. Chudoba
Affiliation:
The University of Texas at Arlington, Arlington, TX76019, USA
*
James.Haley@mavs.uta.edu
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Abstract

The objective of this study is to identify, evaluate, and provide recommendations towards the realisation of near-term hypersonic flight hardware through the consideration of carrier vehicle constraints. The current rush of available funds for hypersonic research cannot cause a program to ignore growth potential for future missions. The prior NB-52 carrier vehicles, famous for the X-15 and X-43A missions, are retired. Next generation hypersonic demonstrator requirements will necessitate a substitution of carrier vehicle capability. Flight vehicle configuration, technology requirements, and recommendations are arrived at by constructing and evaluating a hypersonic technology demonstrator design matrix. This multi-disciplinary parametric sizing investigation of hypersonic vehicle demonstrators focuses on the evaluation of the combined carrier platform, booster, and hypersonic cruiser solution space topography. Promising baseline configurations are evaluated against operational requirements by trading fuel type, endurance cruise time, and payload weight. The multi-disciplinary study results are constrained with carrier payload mass and geometry limitations. The multi-disciplinary results provide physical insights into near-term hypersonic demonstrator payload and cruise time requirements that will stretch the capability of existing carrier aircraft. Any growth in hypersonic research aircraft size or capability will require new carrier vehicle investments.

Keywords

Aerospace designAircraft designHypersonicDemonstrator vehicleCarrier vehicleSizingScramjetModel 176Generic hypersonic vehicleGHVFDL-7Air-breathingRocketX-15X-43X-51
Type
Research Article
Information
The Aeronautical Journal , Volume 124 , Issue 1279 , September 2020 , pp. 1318 - 1349
Copyright
© The Author(s) 2020. Published by Cambridge University Press on behalf of Royal Aeronautical Society

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