B - Operations – Transporting – 64 – G
Patent
B - Operations, Transporting
64
G
B64G 1/14 (2006.01) F02K 9/90 (2006.01) F42B 10/62 (2006.01)
Patent
CA 2706988
The subject of the invention is a spacecraft afterbody device provided with at least one rocket motor (2) at the rear of the craft characterized in that it comprises at least one manoeuvrable cowl element (3, 3a, 3b, 3c, 3d), suitable for taking a first position, for masking and for reducing the rear drag of the craft, where it extends the fuselage of the craft around at least a part of a nozzle (4) of the rocket motor of the craft and stretches beyond the rear of the fuselage of the craft, and for taking a fully deployed second position for increasing the aerodynamic drag of the craft.
L'objet de l'invention est un dispositif d'arrière corps d'engin spatial pourvu d'au moins un moteur fusée (2) à l'arrière de l'engin caractérisé en ce qu'il comporte au moins un élément de capot (3, 3a, 3b, 3c, 3d), manoeuvrable adapté à prendre une première position, de masquage et de réduction de la traînée arrière de l'engin, où il prolonge le fuselage de l'engin autour d'au moins une partie d'une tuyère (4) du moteur fusée de l'engin et s'étend au delà de l'arrière du fuselage de l'engin, et à prendre
Astrium Sas
Bcf Llp
LandOfFree
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