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公开(公告)号:US20190252775A1
公开(公告)日:2019-08-15
申请号:US16276257
申请日:2019-02-14
Applicant: Space Exploration Technologies Corp.
Inventor: Alireza Mahanfar , Javier Rodriguez De Luis
CPC classification number: H01Q3/36 , H01Q1/22 , H05K1/0298 , H05K1/144
Abstract: In one embodiment of the present disclosure, a phased array antenna system includes a first portion carrying an antenna lattice including a plurality of antenna elements, wherein the plurality of antenna elements are arranged in a first configuration, and a second portion carrying a beamformer lattice including a plurality of beamformer elements, wherein the plurality of beamformer elements are arranged in a second configuration different from the first configuration, wherein each of the plurality of antenna elements are electrically coupled to one of the plurality of beamformer elements.
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公开(公告)号:US20190252774A1
公开(公告)日:2019-08-15
申请号:US16276347
申请日:2019-02-14
Applicant: Space Exploration Technologies Corp.
Inventor: Javier Rodriguez De Luis , Robert Baummer, JR. , Nil Apaydin , Alireza Mahanfar
CPC classification number: H01Q3/30 , H01Q1/38 , H01Q3/2658 , H01Q3/267
Abstract: In one embodiment of the present disclosure, a phased array antenna system includes a first portion carrying an antenna lattice including a plurality of antenna elements, wherein the plurality of antenna elements are arranged in a first configuration, a second portion carrying a beamformer lattice including a plurality of beamformer elements, wherein the plurality of beamformer elements are arranged in a second configuration different from the first configuration, and a third portion disposed between the first portion and the second portion carrying at least a portion of a mapping including a first plurality of mapping traces on a first surface providing at least a portion of the electrical connection between the plurality of antenna elements and the plurality of beamformer elements, wherein each of the plurality of antenna elements are electrically coupled to one of the plurality of beamformer elements.
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公开(公告)号:US20180241122A1
公开(公告)日:2018-08-23
申请号:US15898507
申请日:2018-02-17
Applicant: Space Exploration Technologies Corp.
Inventor: Shahrzad Jalali Mazlouman , Kim Schulze
CPC classification number: H01Q3/34 , H01P1/18 , H01Q3/36 , H01Q21/0006 , H01Q21/0075 , H01Q21/061
Abstract: In embodiments, an apparatus includes a two-dimensional (2-D) array of phase shifters including a first plurality of the phase shifters and a second plurality of the phase shifters. The first plurality of the phase shifters is arranged in a first direction of the 2-D array of phase shifters. The first plurality of the phase shifters is electrically connected to a first radio frequency (RF) input. The second plurality of the phase shifters is arranged in a second direction of the 2-D array of phase shifters. The second plurality of the phase shifters is electrically connected to a first radio frequency (RF) output. The first and second directions intersect each other.
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公开(公告)号:US20250141500A1
公开(公告)日:2025-05-01
申请号:US19011384
申请日:2025-01-06
Applicant: Space Exploration Technologies Corp.
Inventor: Martin S. McCormick
IPC: H04B7/0426 , G01S3/56 , H04B7/06 , H04B7/185 , H04B17/318 , H04W16/28 , H04W84/06
Abstract: In an embodiment, a method includes determining a first beam pointing vector associated with an antenna assembly by searching for a satellite from a plurality of satellites. The method includes maintaining a communication link with the satellite by determining a plurality of beam pointing vectors that converge to a signal quality value. The method includes obtaining, from the satellite, satellite ephemeris information of the satellite and one or more of remaining satellites of the plurality of satellites. The method includes determining an estimated orientation of the antenna assembly based on the plurality of beam pointing vectors.
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公开(公告)号:US12273209B2
公开(公告)日:2025-04-08
申请号:US18091748
申请日:2022-12-30
Applicant: Space Exploration Technologies Corp.
Inventor: Joshua S. Salazar , Anno Van den Akker , Robert Ruark , Yong Ren , Bhaskar S. Vadathavoor , Krisztian Bakos
Abstract: In an embodiment, a power delivery system includes a first current limiter and a second current limiter in parallel with each other, wherein a direct current (DC) voltage is provided to each of the first current limiter and the second current limiter; a first transformer electrically coupled to the first current limiter; a second transformer electrically coupled to the second current limiter; first differential signal traces electrically coupled to the first transformer; and second differential signal traces electrically coupled to the second transformer, wherein the DC voltage is transmitted from the first transformer to the first differential signal traces simultaneous with the DC voltage being transmitted to the second differential signal traces by the second transformer.
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公开(公告)号:US12255406B2
公开(公告)日:2025-03-18
申请号:US18242994
申请日:2023-09-06
Applicant: Space Exploration Technologies Corp.
Inventor: Ersin Yetisir
Abstract: An antenna calibration system for a phased array antenna in accordance with one embodiment of the present disclosure generally includes: a beamformer corresponding to a subset of antenna cells of a plurality of antenna cells, wherein the beamformer includes a calibration section for comparing a reference signal to a non-reference signal and a first operating antenna within the subset of antenna cells corresponding with the beamformer. In some implementations, the first operating antenna is configured to deliver a first reference signal (mTx) from the beamformer to be received by a second operating antenna for comparison with a first non-reference signal (Rx) in the beamformer, and/or the first operating antenna is configured to deliver a second non-reference signal (Tx) from a third operating antenna for comparison with a second reference signal (mRx) in the beamformer.
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公开(公告)号:USD1065161S1
公开(公告)日:2025-03-04
申请号:US29891287
申请日:2023-05-03
Applicant: Space Exploration Technologies Corp.
Designer: Anthony Sims , Hubbard D. Velie , Christine Oh , Charlie J. Nitschelm
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公开(公告)号:USD1065160S1
公开(公告)日:2025-03-04
申请号:US29851267
申请日:2022-08-26
Applicant: Space Exploration Technologies Corp.
Designer: Jackson Shaffner , Anthony Sims , Michael J. Conte , Victor Q. Dang , David Milroy , Duncan Edwin Adams
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公开(公告)号:US12218434B2
公开(公告)日:2025-02-04
申请号:US17367140
申请日:2021-07-02
Applicant: Space Exploration Technologies Corp.
Inventor: Ersin Yetisir
Abstract: An antenna assembly in accordance with one embodiment of the present disclosure includes a stack patch antenna assembly defining a plurality of antenna cells made from a plurality of patches, wherein the stack patch antenna assembly includes a first patch layer separated from a second patch layer by a spacer; a beamformer lattice including one or more beamformers, wherein each beamformer corresponds to a subset of antenna cells of the plurality of antenna cells; and a PCB assembly made up from a plurality of layers, the PCB assembly having a feed structure from the stack patch antenna assembly to the beamformer lattice disposed in the PCB assembly, wherein the stack patch antenna assembly is external to the PCB assembly.
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公开(公告)号:US12191941B2
公开(公告)日:2025-01-07
申请号:US18537420
申请日:2023-12-12
Applicant: Space Exploration Technologies Corp.
Inventor: Martin S. McCormick
IPC: H04B7/0426 , H04B7/06 , H04B7/185 , H04B17/318 , H04W16/28
Abstract: In an embodiment, a method includes determining a first beam pointing vector associated with an antenna assembly by searching for a satellite from a plurality of satellites. The method includes maintaining a communication link with the satellite by determining a plurality of beam pointing vectors that converge to a signal quality value. The method includes obtaining, from the satellite, satellite ephemeris information of the satellite and one or more of remaining satellites of the plurality of satellites. The method includes determining an estimated orientation of the antenna assembly based on one or more of the satellite ephemeris information and the plurality of beam pointing vector. The method includes determining a second beam pointing vector based on the estimated orientation, the satellite ephemeris information, and an approximate position information of the antenna assembly.
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