25th AIAA Aerospace Sciences Meeting 1987
DOI: 10.2514/6.1987-448
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Trajectory characteristics of horizontal takeoff single stage to orbit vehicle

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Cited by 6 publications
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“…Horizontal-takeoff single-stageto-orbit (HT-SSTO) has a two dimensional optimal ascent trajectory with aerodynamics and constant thrust which depends on angle of attack and Mach number. The two-dimensional optimal control law can be used in the preliminary design of an arbitrary launch vehicle configuration and provides characteristics of the horizontal-takeoff ascent-to-orbit trajectory [22]. The below figure indicates the diagram of a launch vehicle following the working of SSTO.…”
Section: Single-stage-to-orbit (Ssto)mentioning
confidence: 99%
“…Horizontal-takeoff single-stageto-orbit (HT-SSTO) has a two dimensional optimal ascent trajectory with aerodynamics and constant thrust which depends on angle of attack and Mach number. The two-dimensional optimal control law can be used in the preliminary design of an arbitrary launch vehicle configuration and provides characteristics of the horizontal-takeoff ascent-to-orbit trajectory [22]. The below figure indicates the diagram of a launch vehicle following the working of SSTO.…”
Section: Single-stage-to-orbit (Ssto)mentioning
confidence: 99%