IP Library Granted Patent US 10,320,064
Granted Patent B2
US 10,320,064 · App. 15/364,115 · Granted Jun 11, 2019

Multiport amplifiers (MPAs) using output filtering to improve performance over life

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Quick Facts
Patent No.
US 10,320,064
App. No.
15/364,115
Granted
Jun 11, 2019
Kind
B2
Abstract

A payload subsystem of a satellite includes a plurality of transmit antenna feeds, a plurality of frequency filters, and a power amplification arrangement including a plurality of power amplifiers. The power amplification arrangement has at least one multiport amplifier, the multiport amplifier including a plurality of output ports, each output port coupled with a respective one of the plurality of transmit antenna feeds by way of a respective one of the plurality of frequency filters.

Claims (29)

1. A payload subsystem of a satellite, comprising:

a plurality of transmit antenna feeds, a plurality of frequency filters, and a power amplification arrangement including a plurality of power amplifiers, the power amplification arrangement having at least one multiport amplifier, the multiport amplifier including a plurality of output ports, wherein:

each output port is coupled with a respective one of the plurality of transmit antenna feeds; and

each antenna feed is coupled with a single respective output port by way of a respective one of the plurality of frequency filters.

2. The payload subsystem of claim 1 , wherein the payload subsystem is configured to operate at a frequency band of Ku band or higher.

3. The payload subsystem of claim 1 , wherein the power amplification arrangement is configured to exhibit a ratio of carrier-to-isolation (C/I), between adjacent ones of the plurality of transmit antenna feeds, of at least 30 dB.

4. The payload subsystem of claim 3 , wherein the power amplification arrangement exhibits a C/I, between adjacent ones of the plurality of transmit antenna feeds, of at least 30 dB irrespective of whether calibration of gain and phase variations over life and compensation for the gain and phase variations is performed.

5. The payload subsystem of claim 4 , wherein calibration of the gain and phase variations over life and compensation for the gain and phase variations is avoided.

6. The payload subsystem of claim 3 , wherein the transmit antenna feeds correspond to a coverage map comprising a plurality of coverage regions, wherein adjacent coverage regions are diverse in one or both of channel center frequency and antenna polarization.

7. The payload subsystem of claim 6 , wherein the antenna polarization is diverse in one or both of linear polarization type and circular polarization type.

8. The payload subsystem of claim 1 , wherein:

the payload subsystem further includes a digital channelizer configured to process a plurality of input signals and to create reconfigurable channels to route the plurality of input signals to a plurality of digital channelizer output ports; and

the plurality of digital channelizer output ports are communicatively coupled to the at least one multiport amplifier.

9. The payload subsystem of claim 8 , wherein the at least one multiport amplifier includes a plurality of identical or nearly identical fixed power high power amplifiers (HPAs) whose inputs are communicatively coupled to the plurality of digital channelizer output ports.

10. The payload subsystem of claim 8 , wherein the at least one multiport amplifier includes a plurality of identical or nearly identical variable power high power amplifiers (HPAs) whose inputs are communicatively coupled to the plurality of digital channelizer output ports, wherein output power levels of the variable power HPAs are set and varied approximately in unison.

11. The payload subsystem of claim 1 , wherein at least one of the frequency filters has a rolloff characteristic such that there is 15 dB attenuation between adjacent ones of the plurality of transmit antenna feeds.

12. The payload subsystem of claim 1 , wherein the frequency filters include surface acoustic wave filters.

13. The payload subsystem of claim 1 , wherein the frequency filters are implemented as a band pass filter, a low-pass filter, a high-pass filter, or a serial combination of low-pass and high-pass filters.

14. The payload subsystem of claim 1 , wherein the frequency filters have a passband at least as wide as a channel bandwidth allocated for one of the transmit antenna feeds.

15. The payload subsystem of claim 1 , wherein the power amplifiers are implemented as either SSPAs or TWTAs.

16. A satellite, comprising:

a payload subsystem including a plurality of transmit antenna feeds, a plurality of frequency filters, and a power amplification arrangement including a plurality of power amplifiers, the power amplification arrangement having at least one multiport amplifier, the multiport amplifier including a plurality of output ports, wherein:

each output port coupled with a respective one of the plurality of transmit antenna feeds;

each antenna feed is coupled with a single respective output port by way of a respective one of the plurality of frequency filters; and

the payload subsystem is configured to operate at a frequency band of Ku band or higher.

17. The satellite of claim 16 , wherein the power amplification arrangement is configured to exhibit a ratio of carrier-to-isolation (C/I), between adjacent ones of the plurality of transmit antenna feeds, of at least 30 dB.

18. The satellite of claim 17 , wherein the power amplification arrangement exhibits a C/I, between adjacent ones of the plurality of transmit antenna feeds, of at least 30 dB irrespective of whether calibration of gain and phase variations over life and compensation for the gain and phase variations is performed.

19. The satellite of claim 18 , wherein calibration of gain and phase variations over life and compensation for the gain and phase variations is avoided.

20. The satellite of claim 17 , wherein the transmit antenna feeds correspond to a coverage map comprising a plurality of coverage regions, wherein adjacent coverage regions are diverse in one or both of channel center frequency and antenna polarization.

Assignments (16)
CHANGE OF NAME Recorded Jan 7, 2026
From: MAXAR SPACE LLC
To: LANTERIS SPACE LLC
Reel/Frame 074270/0351 →
CHANGE OF NAME Recorded Nov 6, 2025
From: MAXAR SPACE LLC
To: LANTERIS SPACE LLC
Reel/Frame 073512/0398 →
CHANGE OF NAME Recorded Jun 5, 2023
From: SPACE SYSTEMS/LORAL, LLC
To: MAXAR SPACE LLC
Reel/Frame 063861/0016 →
RELEASE (REEL 060389/FRAME 0720) Recorded May 12, 2023
From: ROYAL BANK OF CANADA
To: MAXAR INTELLIGENCE INC.; MAXAR SPACE LLC
Reel/Frame 063633/0431 →
INTELLECTUAL PROPERTY SECURITY AGREEMENT Recorded May 5, 2023
From: MAXAR INTELLIGENCE INC. (F/K/A DIGITALGLOBE, INC.); AURORA INSIGHT INC.; MAXAR MISSION SOLUTIONS INC. ((F/K/A RADIANT MISSION SOLUTIONS INC. (F/K/A THE RADIANT GROUP, INC.)); MAXAR SPACE LLC (F/K/A SPACE SYSTEMS/LORAL, LLC); SPATIAL ENERGY, LLC; MAXAR SPACE ROBOTICS LLC ((F/K/A SSL ROBOTICS LLC) (F/K/A MDA US SYSTEMS LLC)); MAXAR TECHNOLOGIES HOLDINGS INC.
To: SIXTH STREET LENDING PARTNERS, AS ADMINISTRATIVE AGENT
Reel/Frame 063660/0138 →
TERMINATION AND RELEASE OF SECURITY INTEREST IN PATENTS AND TRADEMARKS - RELEASE OF REEL/FRAME 044167/0396 Recorded May 4, 2023
From: ROYAL BANK OF CANADA, AS AGENT
To: MAXAR INTELLIGENCE INC.; MAXAR SPACE LLC
Reel/Frame 063543/0001 →
TERMINATION AND RELEASE OF PATENT SECURITY AGREEMENT - RELEASE OF REEL/FRAME 060389/0782 Recorded May 4, 2023
From: WILMINGTON TRUST, NATIONAL ASSOCIATION, AS COLLATERAL AGENT
To: MAXAR INTELLIGENCE INC.; MAXAR SPACE LLC
Reel/Frame 063544/0074 →
TERMINATION AND RELEASE OF SECURITY INTEREST IN PATENTS AND TRADEMARKS - RELEASE OF REEL/FRAME 051258/0720 Recorded May 4, 2023
From: ROYAL BANK OF CANADA, AS AGENT
To: MAXAR INTELLIGENCE INC.; MAXAR SPACE LLC
Reel/Frame 063542/0543 →
RELEASE OF SECURITY INTEREST Recorded Jun 21, 2022
From: WILMINGTON TRUST, NATIONAL ASSOCIATION
To: DIGITALGLOBE, INC.; SPACE SYSTEMS/LORAL, LLC; RADIANT GEOSPATIAL SOLUTIONS LLC
Reel/Frame 060390/0282 →
SECURITY AGREEMENT Recorded Jun 17, 2022
From: MAXAR INTELLIGENCE INC.; MAXAR SPACE LLC
To: WILMINGTON TRUST, NATIONAL ASSOCIATION
Reel/Frame 060389/0782 →
SECURITY AGREEMENT Recorded Jun 16, 2022
From: MAXAR INTELLIGENCE INC.; MAXAR SPACE LLC
To: ROYAL BANK OF CANADA
Reel/Frame 060389/0720 →
PATENT SECURITY AGREEMENT Recorded Sep 23, 2020
From: SPACE SYSTEMS/LORAL, LLC
To: WILMINGTON TRUST, NATIONAL ASSOCIATION, AS NOTES COLLATERAL AGENT
Reel/Frame 053866/0810 →
SECURITY AGREEMENT (NOTES) Recorded Dec 12, 2019
From: DIGITALGLOBE, INC.; RADIANT GEOSPATIAL SOLUTIONS LLC; SPACE SYSTEMS/LORAL, LLC (F/K/A SPACE SYSTEMS/LORAL INC.)
To: WILMINGTON TRUST, NATIONAL ASSOCIATION, - AS NOTES COLLATERAL AGENT
Reel/Frame 051262/0824 →
AMENDED AND RESTATED U.S. PATENT AND TRADEMARK SECURITY AGREEMENT Recorded Dec 11, 2019
From: SPACE SYSTEMS/LORAL, LLC
To: ROYAL BANK OF CANADA, AS COLLATERAL AGENT
Reel/Frame 051258/0720 →
SECURITY INTEREST Recorded Oct 5, 2017
From: DIGITALGLOBE, INC.; MACDONALD, DETTWILER AND ASSOCIATES LTD.; MACDONALD, DETTWILER AND ASSOCIATES CORPORATION; MACDONALD, DETTWILER AND ASSOCIATES INC.; MDA GEOSPATIAL SERVICES INC.; SPACE SYSTEMS/LORAL, LLC; MDA INFORMATION SYSTEMS LLC
To: ROYAL BANK OF CANADA, AS THE COLLATERAL AGENT
Reel/Frame 044167/0396 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 7, 2016
From: VADDIPARTY, SUBRAHMANYAM V.; TU, ZHENG; GALLAGHER, VIJAYA KORWAR
To: SPACE SYSTEMS/LORAL, LLC
Reel/Frame 040594/0783 →