GB2508899A - Stripline feed arrangement for antenna sub-arrays - Google Patents

Stripline feed arrangement for antenna sub-arrays Download PDF

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Publication number
GB2508899A
GB2508899A GB1222600.7A GB201222600A GB2508899A GB 2508899 A GB2508899 A GB 2508899A GB 201222600 A GB201222600 A GB 201222600A GB 2508899 A GB2508899 A GB 2508899A
Authority
GB
United Kingdom
Prior art keywords
sub
array
stripline
antenna
support structure
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
GB1222600.7A
Other versions
GB201222600D0 (en
GB2508899B (en
Inventor
Alan Laight
Jonathon James Stafford
Gavin Roy Crouch
Michael Andrew Scott
Paul David Gilliam
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
BAE Systems PLC
Original Assignee
BAE Systems PLC
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by BAE Systems PLC filed Critical BAE Systems PLC
Priority to GB1222600.7A priority Critical patent/GB2508899B/en
Publication of GB201222600D0 publication Critical patent/GB201222600D0/en
Priority to BR112015013853-5A priority patent/BR112015013853B1/en
Priority to PCT/GB2013/053259 priority patent/WO2014091228A1/en
Priority to PL13806040T priority patent/PL2932562T3/en
Priority to US14/651,892 priority patent/US9627776B2/en
Priority to ES13806040T priority patent/ES2698126T3/en
Priority to AU2013357017A priority patent/AU2013357017B2/en
Priority to EP13806040.5A priority patent/EP2932562B1/en
Publication of GB2508899A publication Critical patent/GB2508899A/en
Priority to CL2015001633A priority patent/CL2015001633A1/en
Application granted granted Critical
Publication of GB2508899B publication Critical patent/GB2508899B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00Antenna arrays or systems
    • H01Q21/0006Particular feeding systems
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00Antenna arrays or systems
    • H01Q21/0087Apparatus or processes specially adapted for manufacturing antenna arrays
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00Antenna arrays or systems
    • H01Q21/06Arrays of individually energised antenna units similarly polarised and spaced apart
    • H01Q21/061Two dimensional planar arrays

Abstract

An antenna sub-array 1 comprises a stripline 7 with a plurality of signal pathways branching from a common feed point for signal distribution to a plurality of radiating elements, where the stripline 7 is housed in a support structure located at a distance from a surface of a ground plane 4. The support structure may be formed of a foam material 6 with predefined dielectric properties such as a dielectric constant equal or different to that of air. The support structure may involve channel and button formations arranged to receive the branching stripline 7 antenna feed network. A strong and lightweight support structure 5 may be affixed to the second surface of the ground plane 4. A plurality of antenna sub-arrays may be provided and assembled in a layered arrangement where the sub-arrays are adhesively secured together to form a unitary antenna array. The channels formed in the support structure may be used in a forced cooling system.

Description

IMPROVEMENTS IN ANTENNAS
Field
The present invention relates to the field of antennas, particularly antenna for use in Radar systems. It finds particular, but not exclusive utility in the field of marine Radar systems i.e. those installed on ships.
Background to the present invention
Most or many ships are equipped with at least one Radar system, used for navigation and/or other purposes. In particular, military vessels are frequently equipped with a weapons system Radar which is provided to locate, identify and possibly track possible threats. The complexity and functionality of such a weapons system Radar is far greater than that of a relatively simple navigational Radar system.
In typical prior art systems, the Radar antenna rotates to sweep signals across the location and is affixed to an upper portion of a high mast on the vessel. It is desirable to position the antenna as high as possible to give optimal range coverage and to avoid any other parts of the vessel from obscuring the transmit or receive Radar signal.
A problem with such an arrangement is that the antenna typically has a mass of several hundred kilograms. The mass of the system is due to prior art antennas incorporating a good deal of the Radio Frequency (RF) equipment within the antenna housing. Typically, this RF equipment includes one or more of transmitters, receivers, duplexers, filters and associated processing equipment.
The signals from the RF equipment are passed to digital processing systems, using one or more complex rotating joints which allow electrical continuity between the rotating antenna housing and the connected circuits.
Having a large, heavy rotating mass situated atop a mast, often at the highest point of the vessel, poses problems -not least in terms of stability, installation and maintenance -and there is a general desire to reduce the mass of the rotating part of the Radar system as far as possible. Prior art techniques have tended to concentrate on designing out as much mass from the RE equipment and housing, but there is a limit to how much mass can be eliminated from the antenna housing by these means.
Embodiments of the present invention aim to address these and other problems with prior art Radar antennas, whether mentioned herein or not.
Summary of the Invention
According to an aspect of the present invention, there is provided an antenna sub-array for use in an antenna array comprising a plurality of such sub-arrays, comprising: a stripline for signal distribution, the stripline defining a plurality of signal pathways from a common feed point to a plurality of radiating elements, wherein the stripline is housed in a first support structure located a distance away from a first surface of a ground plane structure.
Preferably. the first support structure comprises a foam material having predefined dielectric properties.
Preferably, the predefined dielectric properties include having a dielectric constant substantially equal to that of air.
Preferably, the stripline is located in a channel in the first support structure and held in position above the first surface of the ground plane structure by a button formed from the same material as the first support structure.
Preferably, affixed to a second surface of the ground plane structure is a second support structure.
Preferably the first and second support structures are different materials.
Preferably, the stripline and the radiating elements are integrally formed.
Preferably, the first support structure comprises a plurality of channels arranged to receive a cooling fluid for cooling the stripline and radiating elements.
According to a further aspect of the present invention, there is provided an antenna array comprising a plurality of sub-arrays according to the first aspect.
According to a still further aspect of the present invention, there is provided a method of manufacturing an antenna array, comprising the steps of: providing a plurality of sub-arrays, each according to the first aspect; assembling the plurality of sub-arrays in a layered arrangement and securing each sub-array to a neighbouring sub-array with an adhesive substance; curing said adhesive to form a unitary antenna array.
According to a still further aspect of the present invention, there is provided a method of cooling an antenna sub-array, according to the first aspect, comprising the steps of: providing a channel in a portion of the sub-array, said channel housing at least some Radio Frequency components; and forcing a cooling fluid into the channel via a first aperture, such that the cooling fluid passes through the channel and is exhausted at a second aperture.
Preferably, the first aperture is proximal to a Radio Frequency connector of the sub-array.
Preferably, the second aperture is proximal to one or more of the plurality of radiating elements.
Preferably the channel is provided in the first support structure, which houses the stripline.
Brief Description of the Figures
For a better understanding of the invention, and to show how embodiments of the same may be carried into effect, reference will now be made, by way of example, to the accompanying diagrammatic drawings in which: Figures la and lb show rear and front views, respectively, of an antenna sub-array according to an embodiment of the present invention; Figure 2 shows a plan view of a stripline in a sub-array according to an embodiment of the present invention; Figure 3 shows a cross-section through a sub-array according to an embodiment of the present invention; Figure 4 shows an front view of an antenna array according to an embodiment of the present invention comprising a plurality of sub-arrays; and Figure 5 shows how a cooling fluid acts to cool the stripline and antenna elements.
Detailed description of preferred embodiment
Embodiments of the present invention allow an antenna array, for use with a Radar system, to be constructed from a plurality of individual sub-arrays. The sub arrays are substantially identical. This provides a great deal of design freedom, and allows antenna arrays having different functional properties to be created, starting from a single building block, namely the sub-array.
The sub-array is arranged to be lightweight and, as such, is constructed, as far as possible, from lightweight foam materials, which are used to support and house the feed and radiating components, which carry and transmit the RF signals, respectively.
At the frequencies used in Radar systems, stripline techniques are often used to carry and distribute the signals from transmitters and/or receivers to individual radiating elements, which are arranged to co-operate to produce a desired antenna performance. Details of the stripline construction and its housing will follow shortly.
Figure la shows a rear perspective view of an antenna sub-array 1 according to an embodiment of the present invention. The sub-array in this embodiment is formed to have a substantially rectangular profile in plan view. In terms of its dimensions, it is significantly larger in width and depth than height, although other configurations are possible where this may not be the case.
On its rear surface, as shown in Figure la, there is provided an RF connector 2 which forms a common feed point for connection of the sub-array 1 to the RE equipment (not shown). The RE connector may be an N-type coaxial connector or any other suitable form of connector.
On the front surface, as shown in Eigure ib, there is provided a plurality of individual radiating elements 3. In the present embodiment, these take the form of identical dipole elements. In alternative embodiments, the individual radiating elements may not be identical and may not be dipole elements, but different forms of antenna.
The dipole elements 3 are integrally formed with the stripline, meaning that the feed structure and the radiating structure are part of the same physical entity, having been milled from the same sheet of material. This has advantages in ease of manufacture and helps to ensure reliable antenna performance.
However, in alternative embodiments, the individual radiating elements may be connected to the stripline feed structure by respective individual connectors.
Figure 2 shows a typical stripline 7 layout. The stripline is milled from sheet aluminium to precise tolerances and, as far as is practicable, from a single sheet of material. The path length of any particular branch is calculated to achieve a particular phase relationship between each respective path. Eor instance, in most cases, it will be desired to ensure that each individual path length is identical and so certain of the individual branches may meander or deviate to achieve this. The exact nature of this meandering not shown here, and will depend on the specification of the antenna sub-array.
The stripline 7 is accommodated as shown in Figure 3 which shows a cross-sectional view through a sub-array 1. On a lower surface of the sub-array, there is a ground plane 4. This is formed from aluminiuml200 foil, 0.2mm thick which is secured to a layer of structural foam 5, by means of a lightweight adhesive film (such as SA7O/lOOg adhesive film). The structural foam 5 provides strength and form to the sub-array. It is chosen to have specified mechanical properties and to be as lightweight as possible, while still providing the required strength and structure. A suitable lightweight structural foam
RT M
material is ROHACELL 31 IG, a polymethacrylimide foam, available from
RTM A
Evonik industries (www.evonik.com).
A
Secured to the upper surface of the structural foam 5, is a further ground plane 4, identical to the one secured to the lower surface of the structural foam 5.
Secured to the upper ground plane 4 is a layer of dielectric foam 6. This is so-called as this layer of foam has specific dielectric properties, which have an influence on the properties of the stripline 7. Specifically, the dielectric foam 6 is selected to have a dielectric constant as near as possible to that of free air. A
RT M
suitable dielectric foam is ROHACELLA31HF, a polymethacrylimide foam, also available from Evonik Industries. In other embodiments, the dielectric foam may be selected to have a dielectric constant which is significantly different to that of free air to achieve different transmission effects.
The same adhesive film, which is used to secure the lower ground plane 4 to the structural foam 5, is used to secure the other parts of the sub-array together i.e. it is located between structural foam 5 an upper ground plane 4, and also between upper ground plane 4 and dielectric foam 6. It is also used to secure each individual sub array to its neighbouring sub-array when the complete array is constructed, as will be described shortly.
The dielectric foam 6 has channels cut into it which conform generally to the arrangement of the stripline 7, such that the stripline 7 can be accommodated in the channels and within the thickness of the dielectric foam 6.
This is illustrated in the detailed view of Figure 3 where a channel in the dielectric foam can be seen, in which is situated the stripline 7. It is supported above the lower ground plane 4 by a button 8 of dielectric foam. There is a similar or identical button 8 positioned above the lower button so that the stripline 7 is effectively sandwiched into position and so can maintain a constant distance between the upper and lower ground planes 4, for its entire length.
This is important in ensuring proper operation of the stripline in feeding RF signals to the antenna elements 3.
The antenna elements 3 are arranged to protrude from beyond the front surface of the sub-array 1.
In order to create an antenna array 10 for use in a Radar system, a plurality of individual sub-arrays 1 are coupled together, as shown in Figure 4.
In this way, the lower ground plane 4 of a first sub-array, when placed atop another sub-array, completes the stripline circuit, by enclosing the stripline 7 between two ground planes.
In order to complete the stripline circuit for the uppermost sub-array, a ground plane 4 is affixed atop the dielectric foam 6. A further layer of structural foam 5 may be provided at the very top of the array to protect the stripline 7 disposed within the uppermost sub-array.
Once the required number of sub-arrays have been assembled, as shown in Figure 4, with an adhesive film being used to couple the various layers together, the entire assembly is cured to form a single unit which is then treated as a single unitary part, since it may not be disassembled without damaging the components contained therein.
The curing process involves placing the complete array assembly in an oven at 80°C. Thermocouples may be provided at various points of the array to ensure that the core temperature is maintained at the correct level. Then the array is allowed to cool, during which time it is found that the height of the array assembly reduces by a few millimetres, typically. However, after about 2 weeks, the height is recovered.
The selected adhesive film having bOg per square metre weight profile ensures that the amount of adhesive in the assembly is a known controlled quantity and allows the stripline and ground plane 4 to interact correctly.
The number of sub-arrays 1 required to form the antenna array 10 is determined by the performance requirements of the finished antenna array.
Using beam-forming techniques, which are know in the field of Radar design, the beams formed by the respective sub-arrays 1 can be made to co-operate to give a desired performance. If a lesser degree of performance is required, then fewer sub-arrays can be included in the antenna array. Therefore, the modular design approach employed herein lends itself well to flexible design methodologies, where overall system requirements can be altered relatively straightforwardly.
Figure 5 shows how the channels formed in the dielectric foam permit a cooling to be propelled through said channels for the purposes of cooling the stripline and radiating elements (not shown in Figure 5, for clarity). Cooled air is the preferred cooling fluid and it is injected into the sub array in the vicinity of the connector 2. The cooled air flows through the channels in which the stripline 7 is housed, and exits the sub-array in the vicinity of the radiating elements 3, having cooled the parts it has contacted along its way. The now warmer air is expelled from the antenna housing in a continuous flow.
The buttons 8 which support the stripline and maintain its position between the upper and lower ground planes are dimensioned to ensure that air can pass through the channels relatively unimpeded. Given the branching nature of the channels, cooling fluid injected at a common point, flows along each channel and cools all parts of the antenna array. The cooling fluid essentially follows the same path as the stripline 7.
By use of the materials and construction techniques disclosed herein, antenna arrays of significantly lower mass than prior art antennas can be constructed. Furthermore, by making use of a plurality of identical sub-arrays, different overall antenna characteristics and specification can be achieved, without re-designing the entire antenna. Instead, the desired performance may be achieved by use of an appropriate number of sub-arrays.
Embodiments of the present invention are able to meet stringent weight requirements by use of composite manufacturing techniques, which are believed not to have been used in antenna manufacture before.
There are no mechanical fixings used in the entire completed array structure, which helps to keep the weight down and reduces possible points of failure. Indeed, the competed array is maintenance free and is considered as a single unit once the manufacturing process is complete.
Attention is directed to all papers and documents which are filed concurrently with or previous to this specification in connection with this application and which are open to public inspection with this specification, and the contents of all such papers and documents are incorporated herein by reference.
All of the features disclosed in this specification (including any accompanying claims, abstract and drawings), and/or all of the steps of any method or process so disclosed, may be combined in any combination, except combinations where at least some of such features and/or steps are mutually exclusive.
Each feature disclosed in this specification (including any accompanying claims, abstract and drawings) may be replaced by alternative features serving the same, equivalent or similar purpose, unless expressly stated otherwise.
Thus, unless expressly stated otherwise, each feature disclosed is one example only of a generic series of equivalent or similar features.
The invention is not restricted to the details of the foregoing embodiment(s). The invention extends to any novel one, or any novel combination, of the features disclosed in this specification (including any accompanying claims, abstract and drawings), or to any novel one, or any novel combination, of the steps of any method or process so disclosed.

Claims (14)

  1. CLAIMS1. An antenna sub-array for use in an antenna array comprising a plurality of such sub-arrays, comprising: a stripline for signal distribution, the stripline defining a plurality of signal pathways from a common feed point to a plurality of radiating elements, wherein the stripline is housed in a first support structure located a distance away from a first surface of a ground plane structure.
  2. 2. The antenna sub-array as claimed in claim 1 wherein the first support structure comprises a foam material having predefined dielectric properties.
  3. 3. The sub-array as claimed in claim 2 wherein the predefined dielectric properties include having a dielectric constant substantially equal to that of air.
  4. 4. The sub-array as claimed in any preceding claim wherein the stripline is located in a channel in the first support structure and held in position above the first surface of the ground plane structure by a button formed from the same material as the first support structure.
  5. 5. The sub-array as claimed in any preceding claim wherein, affixed to a second surface of the ground plane structure is a second support structure.
  6. 6. The sub-array as claimed in claim 5 wherein the first and second support structures are different materials.
  7. 7. The sub-array as claimed in any preceding claim wherein the stripline and the radiating elements are integrally formed.
  8. 8. The sub-array as claimed in any preceding claim wherein the first support structure comprises a plurality of channels arranged to receive a cooling fluid for cooling the stripline and radiating elements.
  9. 9. An antenna array comprising a plurality of sub-arrays, each according to a preceding claim.
  10. 10. A method of manufacturing an antenna array, comprising the steps of: providing a plurality of sub-arrays, each according to any one of claims 1 to 8; assembling the plurality of sub-arrays in a layered arrangement and securing each sub-array to a neighbouring sub-array with an adhesive substance: and curing said adhesive to form a unitary antenna array.
  11. 11. A method of cooling an antenna sub-array, according to any one of claims 1 to 8, comprising the steps of: providing a channel in a portion of the sub-array, said channel housing at least one Radio Frequency component; and forcing a cooling fluid into the channel via a first aperture, such that the cooling fluid passes through the channel and is exhausted at a second aperture.
  12. 12. The method of claim 12 wherein the first aperture is proximal to a Radio Frequency connector of the sub-array.
  13. 13. The method of claim 11 or 12 wherein the second aperture is proximal to one or more of the plurality of radiating elements.
  14. 14. The method of claim 11, 12 or 13 wherein the channel is provided in the first support structure, which houses the stripline.
GB1222600.7A 2012-12-14 2012-12-14 Improvements in antennas Active GB2508899B (en)

Priority Applications (9)

Application Number Priority Date Filing Date Title
GB1222600.7A GB2508899B (en) 2012-12-14 2012-12-14 Improvements in antennas
AU2013357017A AU2013357017B2 (en) 2012-12-14 2013-12-11 Improvements in antennas
PCT/GB2013/053259 WO2014091228A1 (en) 2012-12-14 2013-12-11 Improvements in antennas
PL13806040T PL2932562T3 (en) 2012-12-14 2013-12-11 Improvements in antennas
US14/651,892 US9627776B2 (en) 2012-12-14 2013-12-11 Antennas
ES13806040T ES2698126T3 (en) 2012-12-14 2013-12-11 Improvements in antennas
BR112015013853-5A BR112015013853B1 (en) 2012-12-14 2013-12-11 ANTENNA SUB-ARRANGE, ANTENNA ARRANGEMENT, METHOD OF MANUFACTURING AN ANTENNA ARRANGEMENT, AND, COOLING METHOD OF AN ANTENNA SUB-ARRANGE
EP13806040.5A EP2932562B1 (en) 2012-12-14 2013-12-11 Improvements in antennas
CL2015001633A CL2015001633A1 (en) 2012-12-14 2015-06-11 Antenna Improvement

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1222600.7A GB2508899B (en) 2012-12-14 2012-12-14 Improvements in antennas

Publications (3)

Publication Number Publication Date
GB201222600D0 GB201222600D0 (en) 2013-01-30
GB2508899A true GB2508899A (en) 2014-06-18
GB2508899B GB2508899B (en) 2016-11-02

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GB1222600.7A Active GB2508899B (en) 2012-12-14 2012-12-14 Improvements in antennas

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20180351259A1 (en) * 2017-06-05 2018-12-06 Raytheon Company Electronically scanned array using manifolds

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1990009042A1 (en) * 1989-02-03 1990-08-09 The Secretary Of State For Defence In Her Britannic Majesty's Government Of The United Kingdom Of Great Britain And Northern Ireland Antenna arrays
US5302959A (en) * 1992-02-25 1994-04-12 Hughes Aircraft Company Single element driver architecture for ferrite based phase shifter
US5917456A (en) * 1994-09-02 1999-06-29 Hollandse Signaalapparaten B.V. Stripline antenna
WO2003019723A1 (en) * 2001-08-24 2003-03-06 Andrew Corporation Adjustable antenna feed network with integrated phase shifter
EP1544944A2 (en) * 2003-12-17 2005-06-22 Microsoft Corporation Low-cost, steerable, phased array antenna
WO2008045349A1 (en) * 2006-10-11 2008-04-17 Raytheon Company Antenna array

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL9400165A (en) * 1994-02-03 1995-09-01 Hollandse Signaalapparaten Bv Transmission line network.
EP2395598B1 (en) * 2003-03-04 2018-08-22 Nuvotronics, LLC Coaxial waveguide microstructures and methods of formation

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1990009042A1 (en) * 1989-02-03 1990-08-09 The Secretary Of State For Defence In Her Britannic Majesty's Government Of The United Kingdom Of Great Britain And Northern Ireland Antenna arrays
US5302959A (en) * 1992-02-25 1994-04-12 Hughes Aircraft Company Single element driver architecture for ferrite based phase shifter
US5917456A (en) * 1994-09-02 1999-06-29 Hollandse Signaalapparaten B.V. Stripline antenna
WO2003019723A1 (en) * 2001-08-24 2003-03-06 Andrew Corporation Adjustable antenna feed network with integrated phase shifter
EP1544944A2 (en) * 2003-12-17 2005-06-22 Microsoft Corporation Low-cost, steerable, phased array antenna
WO2008045349A1 (en) * 2006-10-11 2008-04-17 Raytheon Company Antenna array

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20180351259A1 (en) * 2017-06-05 2018-12-06 Raytheon Company Electronically scanned array using manifolds
WO2018226465A1 (en) * 2017-06-05 2018-12-13 Raytheon Company Electronically scanned array using manifolds
US10476168B2 (en) 2017-06-05 2019-11-12 Raytheon Company Electronically scanned array using manifolds

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GB2508899B (en) 2016-11-02

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