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公开(公告)号:US11483021B2
公开(公告)日:2022-10-25
申请号:US17193633
申请日:2021-03-05
Applicant: Space Exploration Technologies Corp.
Inventor: Alireza Mehrnia , Masoud Kahrizi , Alex Ahmad Mirzaei , Bagher Afshar , Ali Sajjadi , Bernd Pregardier , Ka Shun Carson Pun , Omid Nasiby , Igor Elgorriaga
Abstract: In an embodiment, a receiver included in a communications system includes a channel extractor configured to segregate a received signal into a plurality of channel signals, wherein the plurality of channel signals includes a plurality of data signals; and a plurality of decoders electrically coupled to the channel extractor and configured to decode each of the plurality of channel signals into a respective plurality of decoded data beam portions.
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公开(公告)号:US11479372B2
公开(公告)日:2022-10-25
申请号:US17102324
申请日:2020-11-23
Applicant: Space Exploration Technologies Corp.
Inventor: Jonathan F. C. Herman , Stephen Mance , Paul A. Forquera , Mark Krebs
Abstract: A method of communication with a non-GEO constellation of satellites, includes providing an Earth-based terminal configured for communication with a satellite constellation, and establishing communication between the Earth-based terminal and a non-GEO constellation of satellites, the non-GEO constellation of satellites including a first plurality of satellites orbiting at a first inclination, wherein each of the satellites in the first plurality of satellites is in a discrete planar orbit to form a first snake of satellites, the first snake of satellites including adjacent satellites in adjacent orbits having adjacent RAAN (Right Ascension of the Ascending Node), wherein the Earth-based terminal is positioned and configured for continuous communication with at least one satellite from the non-GEO constellation of satellites.
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公开(公告)号:USD963623S1
公开(公告)日:2022-09-13
申请号:US29720096
申请日:2020-01-09
Applicant: Space Exploration Technologies Corp.
Designer: Jackson Shaffner , Anthony Sims , Michael J. Conte , Victor Q. Dang , David Milroy , Duncan Edwin Adams , Ryan Kennett
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公开(公告)号:USD962907S1
公开(公告)日:2022-09-06
申请号:US29720094
申请日:2020-01-09
Applicant: Space Exploration Technologies Corp.
Designer: Jackson Shaffner , Anthony Sims , Ryan Kennett
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公开(公告)号:US20220231691A1
公开(公告)日:2022-07-21
申请号:US17714081
申请日:2022-04-05
Applicant: Space Exploration Technologies Corp.
Inventor: David Francois Jacquet , Mostafa Ghazali , Masoud Kahrizi , Andras Tantos
Abstract: In an embodiment, an apparatus includes an integrated circuit (IC) chip configured to receive a timing signal and a reference clock signal. The IC chips is configured to a reference time signal based on the timing signal and the reference clock signal. The IC chip includes a phase lock loop (PLL). The PLL is synchronized based on the reference time signal.
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公开(公告)号:US20220135258A1
公开(公告)日:2022-05-05
申请号:US17574486
申请日:2022-01-12
Applicant: Space Exploration Technologies Corp.
Inventor: Mohammed Faraz Admani , Pieter Buysschaert , Andrew D. Roberts , Garrett P. Simard
Abstract: Embodiments of the present disclosure are directed to techniques for transitioning a spacecraft from a power-saving state to a power-consuming state at a time after launch of the spacecraft on a launch vehicle. Because the spacecraft can detect conditions for transitioning to the power-consuming state, commands received via an umbilical connection to the launch vehicle, or detecting the presence or absence of such a connection, is unnecessary, thereby removing several technical barriers to eliminating such umbilical connections altogether.
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公开(公告)号:US11322833B2
公开(公告)日:2022-05-03
申请号:US16892231
申请日:2020-06-03
Applicant: Space Exploration Technologies Corp.
Inventor: David Milroy , Victor Q. Dang , Michael J. Conte
IPC: H01Q1/42 , H01Q1/02 , H01Q1/12 , H01Q1/22 , H01Q1/38 , H01Q9/04 , H01Q23/00 , H01Q15/14 , H01Q21/06 , H01Q21/10 , H01Q21/00
Abstract: In one embodiment of the present disclosure, a housing assembly for an antenna apparatus includes a radome portion, a lower enclosure portion, and a fastener system configured for coupling the radome portion and the lower enclosure portion couplable to form an inner compartment for antenna components of an antenna assembly.
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公开(公告)号:US20220069887A1
公开(公告)日:2022-03-03
申请号:US17471098
申请日:2021-09-09
Applicant: Space Exploration Technologies Corp.
Inventor: Nil Apaydin , Chiara Pelletti , Souren Shamsinejad , Alireza Mahanfar
Abstract: In some embodiments, an apparatus includes a plurality of first conductive traces oriented in a first direction in a first layer and plurality of second conductive traces oriented in a second direction in a second layer coupled by vias to define first hierarchical networks. A plurality of third conductive traces oriented in the first direction in a third layer and a plurality of fourth conductive traces oriented in the second direction in a fourth layer are coupled by vias to define second hierarchical networks. Open ends of the first or second traces at a last stage of the first hierarchical networks comprise first ends and open ends of the third or fourth traces at a last stage of the second hierarchical networks comprise second ends. A first end and a corresponding second end are non-collinear to each other and perpendicular to a major plane of the first layer.
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公开(公告)号:US11254451B2
公开(公告)日:2022-02-22
申请号:US15930415
申请日:2020-05-12
Applicant: Space Exploration Technologies Corp.
Inventor: Mohammed Faraz Admani , Pieter Buysschaert , Andrew D. Roberts , Garrett P. Simard
Abstract: Embodiments of the present disclosure are directed to techniques for autonomously transitioning a spacecraft from a power-saving state to a power-consuming state at a time after launch of the spacecraft on a launch vehicle. Because the spacecraft can autonomously detect conditions for transitioning to the power-consuming state, commands received via an umbilical connection to the launch vehicle, or detecting the presence or absence of such a connection, is unnecessary, thereby removing several technical barriers to eliminating such umbilical connections altogether. In some embodiments, low-cost vacuum detection devices that use very small amounts of power may be used by the spacecraft to detect when the spacecraft has reached an altitude suitable for transitioning to the power-consuming state.
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公开(公告)号:US20220006610A1
公开(公告)日:2022-01-06
申请号:US17478599
申请日:2021-09-17
Applicant: Space Exploration Technologies Corp.
Inventor: Andras Tantos , David Francois Jacquet , Mario Toma
IPC: H04L7/033
Abstract: In an embodiment, an apparatus includes an integrated circuit (IC) chip configured to receive a timing signal and a reference clock signal and generate a first reference time signal based on the timing signal and the reference clock signal. The IC chip includes a clock phase lock loop (PLL) configured to generate and provide a second reference clock signal at a higher frequency than the reference clock signal; the IC chip is further configured to generate a second reference time signal based on the first reference time signal and the second reference clock signal. The second reference time signal specifies a count of a number of cycles of the second reference clock signal starting from a particular cycle of the second reference clock signal. The second reference time signal has a finer count resolution than the first reference time signal for a same time period.
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