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

Bibliographische Detailangaben

Hauptverfasser:	HETHCOCK, JR., James Donn, WYATT, Robert David, GAMON, Jeffrey A, GILCHRIST, Ian, LEVY, David W, DERMAN, Michael, VAN BAVEL, Luc, KOEHLER, Dieter, MATARRESE, Michael, Thompson, Luke A
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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