@inproceedings{a16b7a4bf8874abb81859547d23bbd37,
title = "Mission abort trajectories of orbital stage with maximum longitudinal and lateral ranges",
abstract = "Mission abort scenarios of the orbital stage of a two-stage space transportation system due to an engine failure are considered. The gliding flight which the orbital stage performs to reach an emergency landing site is treated as a maximum range problem for longitudinal and lateral directions. Thus, the reachable area can be determined. With the use of the orbital maneuvering system, the range can be significantly increased.",
author = "M. Mayrhofer and \{da Costa\}, O. and G. Sachs",
year = "2003",
doi = "10.2514/6.2003-7078",
language = "English",
isbn = "9781624100857",
series = "12th AIAA International Space Planes and Hypersonic Systems and Technologies",
publisher = "American Institute of Aeronautics and Astronautics Inc.",
booktitle = "12th AIAA International Space Planes and Hypersonic Systems and Technologies",
note = "12th AIAA International Space Planes and Hypersonic Systems and Technologies 2003 ; Conference date: 15-12-2003 Through 19-12-2003",
}