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公开(公告)号：US20170029138A1
公开(公告)日：2017-02-02
申请号：US15303898
申请日：2015-04-03
Applicant: CENTRE NATIONAL D'ETUDES SPATIALES
Inventor： Pascal Bultel
CPC classification number: B64G1/007 , B64G1/402 , B64G1/646 , B64G2001/1092
Abstract: The invention relates to a method for transferring a space payload from a first orbit to a second orbit. Said method is characterized in that the space payload, moving about the first orbit, is attached to a removable orbital towing assistance device including at least one fuel pouch. Said method includes the steps of: —attaching (E1) an orbital transfer vehicle to the removable orbital towing assistance device; and —transferring (E2) the space payload and the removable orbital towing assistance device to the second orbit by means of the orbital transfer vehicle. The invention also relates to a removable orbital towing assistance device intended for a space payload and an orbital transfer vehicle and enabling direct supply of fuel to the vehicle and/or the space payload.
Abstract translation: 本发明涉及一种将空间有效载荷从第一轨道传送到第二轨道的方法。 所述方法的特征在于，围绕第一轨道移动的空间有效载荷附接到包括至少一个燃料袋的可拆卸轨道牵引辅助装置。 所述方法包括以下步骤：将轨道转移车辆（E1）附接到可拆卸轨道牵引辅助装置; 并通过轨道转运车辆（E2）将空间有效载荷和可移动轨道牵引辅助装置（E2）传送到第二轨道。 本发明还涉及一种用于空间有效载荷和轨道转运车辆并且能够直接向车辆和/或空间有效载荷提供燃料的可拆卸的轨道牵引辅助装置。
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公开(公告)号：US20150001347A1
公开(公告)日：2015-01-01
申请号：US14346098
申请日：2012-09-20
Applicant: CENTRE NATIONAL D'ETUDES SPATIALES
Inventor： Pascal Bultel
CPC classification number: B64G1/40 , B64G1/007 , B64G1/242 , B64G1/405 , B64G1/406 , B64G1/42 , B64G1/422 , B64G1/428 , B64G1/44 , B64G1/443 , B64G1/503 , B64G1/64 , B64G1/641
Abstract: This invention relates to a propulsion bay to be transported, at least temporarily, in a space launch vehicle and comprising an adapter that co-operates with at least one system located, at least temporarily, on board the bay, said system comprising an electrical power supply. The bay is characterized in that it also comprises at least one electric space propulsion engine that can be powered by the power supply of the system.
Abstract translation: 本发明涉及至少暂时在空间运载火箭中运输的推进舱，并包括一个适配器，该适配器与至少临时位于船上的至少一个系统协同工作，所述系统包括电力 供应。 其特征在于它还包括至少一个电动空间推进发动机，其可以由系统的电源供电。
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公开(公告)号：US10858124B2
公开(公告)日：2020-12-08
申请号：US15303898
申请日：2015-04-03
Applicant: CENTRE NATIONAL D'ETUDES SPATIALES
Inventor： Pascal Bultel
Abstract: The invention relates to a method for transferring a space payload from a first orbit to a second orbit. Said method is characterized in that the space payload, moving about the first orbit, is attached to a removable orbital towing assistance device including at least one fuel pouch. Said method includes the steps of: —attaching (E1) an orbital transfer vehicle to the removable orbital towing assistance device; and —transferring (E2) the space payload and the removable orbital towing assistance device to the second orbit by means of the orbital transfer vehicle. The invention also relates to a removable orbital towing assistance device intended for a space payload and an orbital transfer vehicle and enabling direct supply of fuel to the vehicle and/or the space payload.
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公开(公告)号：US09963250B2
公开(公告)日：2018-05-08
申请号：US14346098
申请日：2012-09-20
Applicant: CENTRE NATIONAL D'ETUDES SPATIALES
Inventor： Pascal Bultel
CPC classification number: B64G1/40 , B64G1/007 , B64G1/242 , B64G1/405 , B64G1/406 , B64G1/42 , B64G1/422 , B64G1/428 , B64G1/44 , B64G1/443 , B64G1/503 , B64G1/64 , B64G1/641
Abstract: This invention relates to a propulsion bay to be transported, at least temporarily, in a space launch vehicle and comprising an adapter that co-operates with at least one system located, at least temporarily, on board the bay, said system comprising an electrical power supply. The bay is characterized in that it also comprises at least one electric space propulsion engine that can be powered by the power supply of the system.
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