Method and apparatus for missile interface testing

Details Method and apparatus for missile interface testing Method and apparatus for missile interface testing

G - Physics

01

R

G01R 31/3177 (2006.01) F41G 7/00 (2006.01) G06F 17/50 (2006.01)

Patent

CA 2100156

An apparatus (10) for testing an operational status of a missile interface system includes a portable control unit (16) having an interface panel (28). The interface panel (28) has a plurality of umbilical ports adapted to receive data from a plurality of missile stations (12) via a corresponding plurality of umbilical cables (18). The interface panel (28) is further includes a coaxial port (40), adapted to receive data from a radar trap (22) via a coaxial cable (20). The apparatus further includes a fixture assembly (116) having a main body portion (120). The main body portion (120) has a channel (122) through which a first end of the umbilical cable (18) is allowed to pass. The fixture assembly (116) is adapted to be releasably mounted to a missile station (12).

La présente invention a pour objet un dispositif (10) servant à la situation opérationnelle d'un système d'interface pour missile, comportant un module de commande portatif (16) avec panneau d'interface (28). Le panneau d'interface (28) comporte une pluralité de prises ombilicales destinées à recevoir les données provenant d'une pluralité d'emplacements de missiles (12) et transmises par l'intermédiaire d'une pluralité de câbles ombilicaux (18). Le panneau d'interface (28) comporte en outre une prise coaxiale (40) destinée à la réception de données provenant d'un détecteur de radar (22) et transmises par l'intermédiaire d'un câble coaxial (20). Le dispositif comporte en outre un boîtier (116) et un corps principal (120). Le corps principal (120) comporte une voie de passage (122) traversée par une première extrémité du câble ombilical. Le boîtier (116) se prête au montage sur les emplacements de missiles (12).

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