Universal spacecraft separation node
AssigneeLockheed Martin Corporation
InventorsMark Kaszubowski, Christopher Kerley
Life of this patent
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AssigneeLockheed Martin Corporation
InventorsMark Kaszubowski, Christopher Kerley
Estimating the term…
An integrated separation system and interface structure is disclosed for a variety of deployment applications. In one embodiment, a Universal Spacecraft Separation Node (100) includes a separation nut assembly (102), a separation spring assembly (104) an LV node fitting (106) and an SC node fitting (108). The LV node fitting (106) is connected to a launch vehicle (210) and the SC node fitting (108) is connected to a spacecraft (216). The separation nut assembly (102) holds the fittings (106 and 108) together until separation is desired. Upon separation, the separation spring assembly (104) provides a force to urge the launch vehicle (210) and spacecraft (216) apart. Prior to separation, an annular tongue (224) of fitting (108) mates with an annular groove (226) of fitting (106) to resist shear forces.
An apparatus for use in selectively connecting one or more deployable payloads and a dispenser, each said deployable payload including a payload surface and said dispenser including a dispenser surface wherein, prior to deployment of said payload, said payload surface and dispenser surface are disposed in opposing relationship, said payload being deployable from an undeployed state wherein said payload surface and dispenser surface are disposed proximate to one another and a deployed state wherein said payload surface and dispenser surface are separated, said apparatus comprising:
An apparatus for use in selectively connecting one or more deployable payloads and a dispenser, each said deployable payload including a payload surface and said dispenser including a dispenser surface wherein, prior to deployment of said payload, said payload surface and dispenser surface are disposed in opposing relationship, said payload being deployable from an undeployed state wherein said payload surface and dispenser surface are disposed proximate to one another and a deployed state wherein said payload surface and dispenser surface are separated, said apparatus comprising:
An apparatus for use in selectively connecting one or more deployable payloads and a dispenser, each said deployable payload including a payload surface and said dispenser including a dispenser surface wherein, prior to deployment of said payload, said payload surface and dispenser surface are disposed in opposing relationship, said payload being deployable from an undeployed state wherein said payload surface and dispenser surface are disposed proximate to one another and a deployed state wherein said payload surface and dispenser surface are separated, said apparatus comprising:
An apparatus for use in selectively connecting one or more deployable payloads and a dispenser, each said deployable payload including a payload surface and said dispenser including a dispenser surface wherein, prior to deployment of said payload, said payload surface and dispenser surface are disposed in opposing relationship, said payload being deployable from an undeployed state wherein said payload surface and dispenser surface are disposed proximate to one another and a deployed state wherein said payload surface and dispenser surface are separated, said apparatus comprising:
Dependencies are inferred from the claim text.