Flyback of the SPARTAN Scramjet-Powered Launch Vehicle
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[1] Michael J. Aftosmis,et al. Adjoint-based low-boom design with Cart3D (Invited) , 2011 .
[2] I. Michael Ross,et al. Direct trajectory optimization by a Chebyshev pseudospectral method , 2000, Proceedings of the 2000 American Control Conference. ACC (IEEE Cat. No.00CH36334).
[3] Gediminas Adomavicius,et al. A Parallel Multilevel Method for Adaptively Refined Cartesian Grids with Embedded Boundaries , 2000 .
[4] Markus Kuhn,et al. Innovative European Launcher Concept SMILE , 2017 .
[5] U. M. Schottle,et al. Comparison of Glideback and Flyback Boosters , 2001 .
[6] Takeshi Tsuchiya,et al. Optimal Design of Two-Stage-To-Orbit Space Planes with Airbreathing Engines , 2005 .
[7] David Evans,et al. Vehicle and mission design of a future small payload launcher , 2017 .
[8] Tetsuo Hiraiwa,et al. Evaluation of Effectiveness of Periodic Flight by a Hypersonic Vehicle , 2007 .
[9] Katharine Smith,et al. Launch and deployment of distributed small satellite systems , 2015 .
[10] Barry M. Hellman,et al. Comparisons of Measured and Modeled Aero-thermal Distributions for Complex Hypersonic Configurations , 2017 .
[11] I. Michael Ross,et al. Pseudospectral Knotting Methods for Solving Optimal Control Problems , 2004 .
[12] Alan W. Wilhite. Technology and staging effects on two-stage-to-orbit systems , 1994 .