Aircraft Design and Technology

An aircraft designed to provide sustained G forces, with a relatively high steady angle of attack maneuverability using less thrust by balancing thrust and drag to sustain a high turn rate with dual low thrust engines using novel wing and fuselage designs. The aircraft includes a wing oriented later...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Koehler, Dieter, Hethcock, JR., James Donn, Levy, David W, Van Bavel, Luc, Gamon, Jeffrey A, Wyatt, Robert David, Gilchrist, Ian, Matarrese, Michael, Derman, Michael, Thompson, Luke A
Format: Patent
Sprache:eng
Schlagworte:
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