Apparatus for the controlled advance and retraction of a flexibl

Aeronautics and astronautics – Missile stabilization or trajectory control – Remote control

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244158R, B64G 138

Patent

active

044362595

ABSTRACT:
This invention relates to an improvement in an apparatus for advancing or retracting a flexible pay-out connection in a controlled manner, for instance a pay-out cable fixed to a satellite body with a pay-out means mounted thereon, in particular for a spin-imparted satellite, the improvement comprising at least one groove means at the periphery of the satellite body to receive the pay-out connection, and at least one elastic holding means to hold the pay-out connection at the groove opening.

REFERENCES:
patent: 3229930 (1966-01-01), Fedor et al.
patent: 3277486 (1966-10-01), Kuebler
patent: 3715092 (1973-02-01), Moyer et al.
patent: 4350315 (1982-09-01), Pollin

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