Apparatus with axis-parallel tension cables for ejecting a spin-stabilized body from a spacecraft
AssigneeEADS Space Transportation GmbH
InventorHorst Koehler
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AssigneeEADS Space Transportation GmbH
InventorHorst Koehler
Estimating the term…
An apparatus for ejecting a flying body (e.g. payload recovery container) from a spacecraft includes a first ring to be secured to the spacecraft, a cable winding device that is arranged on a second ring and that is releasably engageable with the flying body, and tension cables extending between the two rings. The cable winding device is spring-biased to wind-up the cables, which extend axis-parallel along the cylindrical outer shell of the flying body. Holding and guide elements on the first ring hold and guide the flying body. Catch elements on the cable winding device releasably engage receivers on the flying body. When the holding elements are released, the cables are retracted by the cable winding device, and the rotation of the cable winding device is transmitted to the flying body via the engaged catch elements and receivers. Thereby, the flying body is rotated and translationally ejected.
An apparatus for ejecting a spin-stabilized flying body from a spacecraft, said apparatus comprising:
A spacecraft system comprising a spacecraft having an ejection bay, a flying body that is received in said ejection bay and that is to be ejected in a spin-stabilized manner out of said ejection bay, and an ejection apparatus that is arranged in said ejection bay and that is adapted to eject said flying body with a translation motion and a rotation motion out of said ejection bay, wherein said ejection apparatus comprises:
Dependencies are inferred from the claim text.