通信ペイロード

衛星観測機器:テキサス・インスツルメンツ製トランスポンダ・ソリューション

設計上の考慮事項

In a communications satellite, a Transponder gathers signals over a range of uplink frequencies and re-transmits them on a different set of downlink frequencies to receivers on Earth, often without changing the content of the received signal or signals. Multiple transponders are found on every satellite payload system operating in the C, extended C , S and Ku-bands.

The top considerations for space designs are power, size, weight, and performance. Thermal performance is critical in high power devices. Due to the environment, cooling is done through conduction. As power components increase their efficiency and shrink their footprint, the trend is to move towards distributed power systems which allow the insertion of more point of load DC to DC convertors. As voltages decrease, noise margins become more critical, thus increasing the need for low noise supplies and driving the need for lower drop out regulators situated near the load. Models (IBIS for digital parts, Pspice for analog parts) are often used to analyze the design. Design functionality can be broken up in multiple blocks or circuit cards and maybe done by separate designers or even subcontracted to another company.

To promote reliability, floating metal is often not allowed in long term applications. Floating inputs are avoided and No Connect pins are strongly scrutinized. Overshoot/Undershoot conditions are analyzed to ensure IC’s are not overly stressed. Insertion of new technology is difficult due to multiple reasons: budget, analysis effort, qualification, and trust in proven way of doing things. This can be overcome by solving design critical issues such as: power, performance, reliability and footprint. Designs are often done in multiple board spins offering multiple chances for technology insertion into the final flight design (Prototype, EM/EDU, and Flight). Oftentimes product availability is met through criteria such as: redundancy, self-checking, TMR schemes, error checking.

Ionizing radiation found in natural space environments can strongly affect the operation of electronic circuits used in space applications. HiRel performs total dose testing on space-qualified, QML Class-V new product releases in order to determine how much radiation our devices can absorb before device degradation occurs. The test results for select devices are available at www.ti.com/radiation .

技術資料

アプリケーション・ノート

アプリケーション・ノート (3)

タイトル 概要 種類 サイズ (KB) 日付 表示回数 英語版
PDF 415 KB 2018年 8月 1日 0
PDF 350 KB 2018年 7月 31日 0
PDF 796 KB 2018年 7月 27日 0

セレクション/ソリューション・ガイド

セレクション・ガイド (1)

タイトル 概要 種類 サイズ (KB) 日付 表示回数 英語版
PDF 1.24 MB 2014年 7月 8日 266

サポートとトレーニング

TI のサポート・フォーラムをお試しください
このパーツに関連するエキスパートからの回答の検索 新しい質問の投稿

コミュニティ内のコンテンツは、個別の TI 投稿者やコミュニティ投稿者によって「現状のまま」提供されるもので、TI による仕様の追加を意図するものではありません。
使用条件をご確認ください。

その他のサポート

ニュース・リリース/寄稿記事

Blogs