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Innovative Lightweight Antenna Array for Space

A new flexible antenna design enhances space communication capabilities.

― 5 min read


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Large antennas in space are essential for high-power and high-speed communication. They are needed for tasks such as wireless power transfer and data transmission. However, creating these antennas is challenging because they must fit into the limited space of a rocket during launch. This article discusses a new type of lightweight and FlexibleAntenna Array designed to overcome these difficulties.

The Need for Large Antennas in Space

Space applications, such as solar power collection and advanced Communication Systems, require antennas with large surfaces. These antennas must be capable of producing strong signals and handling high amounts of data. The challenge is that large antennas need to be stored in a compact form to fit within the rocket.

Current designs for portable antennas often involve options like foldable or inflatable types. Yet, these solutions have limitations, generally only allowing for sizes of a few square meters. This is inadequate for the ambitious demands of future satellite systems and space solar power projects.

The Design of a Flexible Antenna Array

The new antenna array is made of dipole antennas attached to a composite material that is light and flexible. This design allows the array to change shape and fold flat for transport. When deployed, it can pop back into its intended shape. The materials chosen for this array also allow for efficient mass production, a necessary step for creating large numbers of antennas to cover big areas in space.

The antennas have been rigorously tested to ensure they can withstand the harsh conditions of space travel. They are designed to endure mechanical shocks, extreme temperatures, and the pressure changes that come with launch and operation in orbit. In addition, these antennas show excellent performance in terms of signal transmission.

Manufacturing and Assembly Process

The construction of these antennas is crucial. They are made from a flexible sheet of polyimide with copper layers. This material choice keeps the antenna lightweight while allowing it to maintain flexibility. Rather than using traditional hard materials, polyimide can bend and return to its shape when needed.

The assembly includes attaching this conductive sheet to a frame made from glass fiber. This frame is shaped into a "J" form, providing a robust structure that can still be flexible. A special method called "co-curing" fuses these two layers together during the manufacturing process, ensuring a reliable and solid bond.

Electromagnetic Characteristics

Each antenna consists of a few essential components: a circuit board, a transmission line, and two radiating arms. The transmission line is particularly important as it connects the antenna to the rest of the system and ensures that the signal is sent and received correctly. The design allows for effective matching of electrical impedance, which is vital for excellent signal quality.

The antennas have been simulated in various configurations to test their performance. The results show that the antennas can operate efficiently over a wide frequency range, making them suitable for diverse applications.

Mechanical Performance and Testing

Space missions can be incredibly tough on equipment, exposing it to vibrations and temperature swings. To ensure the antennas can handle these conditions, extensive testing was carried out. The antennas underwent numerous tests to check their Durability against vibrations, thermal cycling, and storage conditions.

During these tests, the antennas were subjected to both high and low temperatures, repeated cooling in liquid nitrogen, and even vibrations mimicking rocket launches. Remarkably, the antennas showed no signs of damage, proving their reliability for deployment in challenging environments.

Thermal Limits and Cycling

Spacecraft experience significant temperature changes, especially when orbiting the Earth and moving in and out of sunlight. To simulate these conditions, the antennas went through thermal cycling tests that exposed them to rapid temperature changes.

During these tests, the antennas were placed in a vacuum chamber to replicate the lack of atmosphere in space. They underwent cycles of extreme cooling and heating to ensure they could withstand the harsh realities of space missions. Once again, the antennas performed well, showing no significant issues after the tests.

Long-term Stowage Testing

In space, equipment often needs to be stored for long periods before deployment. This requires the materials to maintain their integrity over time. To address this, a special testing method was employed that simulated long stowage periods in a shorter timeframe.

The array was flattened and exposed to elevated temperatures to mimic months of waiting time. The results were positive; the antennas returned to their intended shape without any loss in performance. This indicates that they can be stored for extended periods without compromising their functionality.

Applications Beyond Space

Although the antennas are specifically designed for space missions, their features make them suitable for various other uses on Earth. For example, their lightweight and flexible design could benefit communication systems in remote or challenging locations.

These antennas could be significant in fields like robotics, remote sensing, or even maritime applications where space and weight constraints are crucial. Their ability to perform well even after exposure to harsh conditions opens opportunities for innovative solutions outside of traditional settings.

Conclusion

The creation of a lightweight and flexible antenna array marks a promising advancement in the field of space engineering. By addressing the challenges of deploying large antennas in space, these designs can help enhance communication and energy systems in the future.

As technology progresses, there is hope that these antennas will pave the way for more innovative approaches in various fields, improving efficiency and capabilities. The flexibility in design and production also supports various applications beyond space, showing the potential for these antennas to impact a broad range of technologies.

Continuing to refine these methods and materials will likely lead to even greater advancements in the field. The future holds exciting possibilities for lightweight, durable, and efficient antenna systems.

Original Source

Title: Popup Arrays for Large Space-Borne Apertures

Abstract: Large apertures in space are critical for high-power and high-bandwidth applications spanning wireless power transfer (WPT) and communication, however progress on this front is stunted by the geometric limitations of rocket flight. Here, we present a light and flexible 10GHz array, which is composed of dipole antennas co-cured to a glass-fiber composite. The arrays are designed to dynamically conform to new shapes and to be flexible enough to fold completely flat, coil, and pop back up upon deployment. The design was chosen to be amenable to scalable, automated manufacturing - a requirement for the massive production necessary for large apertures. Moreover, the arrays passed the standard gamut of required space-qualification testing: the antennas can survive mechanical stress, extreme temperatures, high-frequency temperature cycling, and prolonged stowage in the flattened configuration. The elements exhibit excellent electromagnetic performance - with a return ratio better than -10dB over a bandwidth of 1.5GHz and a single lobe half-power beam width of greater than $110^\circ$ suitable for broad range beamforming and with excellent manufacturing consistency. Moreover, its mechanical durability vis-a-vis extreme temperatures and protracted stowage lends itself to demanding space applications. This lightweight and scalable array is equipped to serve a host of new space-based radio-frequency technologies and applications which leverage large, stowable and durable array apertures.

Authors: Oren S. Mizrahi, Austin Fikes, Alan Truong, Fabian Wiesemüller, Sergio Pellegrino, Ali Hajimiri

Last Update: 2023-08-14 00:00:00

Language: English

Source URL: https://arxiv.org/abs/2308.07458

Source PDF: https://arxiv.org/pdf/2308.07458

Licence: https://creativecommons.org/licenses/by/4.0/

Changes: This summary was created with assistance from AI and may have inaccuracies. For accurate information, please refer to the original source documents linked here.

Thank you to arxiv for use of its open access interoperability.

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