Hughes Aircraft Company

Kevin S Minds

Dzung V Phan

Leonard Ellman

A combination connector (20) includes a first half connector (22) with a fixed central body (40) and a slidable exterior housing (54) that is biased to a first position, and a second half connector (24) with a fixed exterior housing (70) and a slidable interior body (82) that is biased to a first position. The fixed central body (40) of the first half connector (22) has electrical contacts (42) on its periphery, and the fixed exterior housing (70) has electrical contacts on its interior wall. The slidable exterior housing (54) of the first half connector (22) protects the connection points before the connection is made, and is pushed back to expose the connection points as the two connectors are mated together. The slidable interior body (82) of the second half connector (24) includes a shorting ring (88) that shorts out the electrical contacts (74) of the second half connector (24) before the connection is made, and is pushed back to expose the electrical contacts (74) when the first and second half connectors (22, 24) are mated. One half of a fiber optic cable (48) extends longitudinally through the fixed central body (40) of the first half connector (22), and the other half of the optical cable (80) extends longitudinally through the second half connector (24), and the two are placed into axial contact when the two halves (22, 24) are brought together. The first and second half connectors (22, 24) are dimensioned to ensure registration of the appropriate parts as they are pushed together.

Combination optical fiber and electrical connector

A missile launching system with an open-ended cylindrical container (10) having a bore in which a slidable piston (20) is located between the missile (12) and a gas generator (14) adjacent the container aft end (16). The piston (20) area is substantially the same as the container bore at the aft end (16). An internal ring (42) forms a reduced area throat for gas exiting via the aft end of the container (10) with the ratio of the piston area to the throat area, A.sub.p /A.sub.t, being functionally related to the propellant physical characteristics.

Growing community of inventors

West Hills, CA, United States of America

Kevin S Minds