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MOTOCICLETA-AVION ULTRALIGERO. COMPRENDE DOS ESTRUCTURAS: LA DE UNA MOTOCICLETA TODO TERRENO, CON TODOS SUS ELEMENTOS NORMALES, Y POR OTRA LA SUSTENTADORA DE UN AVION ULTRALIGERO, QUE UNIDAS COMPARTEN EL MISMO MOTOR QUE ES EL DE LA MOTOCICLETA, PARA PROPULSAR EL APARATO EN EL AIRE, O PROPULSAR LA MOTOCICLETA EN TIERRA; SIENDO LA ESTRUCTURA DE VUELO DE TIPO <CANARD>, FORMADA POR UN TUBO LONGITUDINAL (1) AL QUE ESTAN UNIDAS TRANSVERSALMENTE EL ALA (B) Y EL ESTABILIZADOR HORIZONTAL (C), INCLUYENDO EL TIMON DE DIRECCION (P), ESTANDO FORMADA EL ALA (B) POR DOS LARGUEROS SOLAMENTE Y POR CUATRO TRAVESAÑOS, QUE JUNTO AL TUBO LONGITUDINAL (A) Y LOS CABLES SUJETOS A LOS PUNTOS (A, B, C, E, F) FORMAN UN CONJUNTO SUFICIENTEMENTE RIGIDO PARA EL VUELO, HABIENDOSE INCLUIDO ADEMAS EN LOS EXTREMOS DE LAS ALAS, PATINES (H) UTILES PARA EVITAR QUE LA PUNTA ALAR ROCE CON EL SUELO.
A short description of the NAE airborne simulator feel system(Single channel wheel system with electrohydraulic servoactuators for flight control feel system)
A study of the effects of parameter variation on the flying qualities of the XV-4 B V/STOL aircraft(Effects of variations in stability derivatives on performance of XV-4 aircraft)[Technical Report, Oct. 1967- Oct. 1969]