Three=axis steering aircraft of canard type

The rear fin and rudder assembly (19) is V-shaped, while the propeller circle (4) is covered on the down side by fins (3). The fuselage (1) support is in the form of a lattice frame (5), with the cross-beam (2) forming part of the frame. Pref., the aircraft fuselage has a triangular configuration in...

Ausführliche Beschreibung

Bibliographische Detailangaben

1. Verfasser:	SCHLACHTER, MANFRED, 67133 MAXDORF, DE
Format:	Patent
Sprache:	eng ; ger
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
Online-Zugang:	Volltext bestellen
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