A missile or rocket comprising two parts which are separable along trajectory

A missile or rocket comprising two parts which are separable along trajectory

A flying machine, particularly a missile, comprising two parts (20, 30), a front part (20) and a rear part (30) respectively, intended to be separated along trajectory, characterized in that it further comprises an asymmetric canopy (50) linked to the rear part (30) and making it possible to ensure...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: PHILIPPE MOURRY, MARC PINOL
Format: Patent
Sprache:eng
Schlagworte:
AMMUNITION
BLASTING
EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
HEATING
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
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Beschreibung
Zusammenfassung:A flying machine, particularly a missile, comprising two parts (20, 30), a front part (20) and a rear part (30) respectively, intended to be separated along trajectory, characterized in that it further comprises an asymmetric canopy (50) linked to the rear part (30) and making it possible to ensure divergence between the trajectories of the two parts.