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First Evaluation Of The Main Parameters In The Dynamics Of The Small Expendable Deployer System (seds) For A Tethered Satellite by L. De Luca

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1NASA Technical Reports Server (NTRS) 19910000785: First Evaluation Of The Main Parameters In The Dynamics Of The Small Expendable Deployer System (SEDS) For A Tethered Satellite

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The dynamics of the motion of the Small Expendable Deployer System (SEDS) is studied by using a simplified model in which no external forces (except the gravity gradient field) are applied on the tethered body and the tether is assumed massless. The dynamics of SEDS operation is modeled as a sequence of two phases: the deployment phase and the swing phase. For the first one the velocity dependent forces are found to force the tether forward from the local vertical. When the deployment ends, Coriolis effects vanish and the swing phase begins, which is characterized by a wide free libration. The time duration as well as velocity, acceleration and tension of the tethered body are estimated for both deployment and swing phases.

“NASA Technical Reports Server (NTRS) 19910000785: First Evaluation Of The Main Parameters In The Dynamics Of The Small Expendable Deployer System (SEDS) For A Tethered Satellite” Metadata:

  • Title: ➤  NASA Technical Reports Server (NTRS) 19910000785: First Evaluation Of The Main Parameters In The Dynamics Of The Small Expendable Deployer System (SEDS) For A Tethered Satellite
  • Author: ➤  
  • Language: English

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The book is available for download in "texts" format, the size of the file-s is: 20.54 Mbs, the file-s for this book were downloaded 59 times, the file-s went public at Sun Sep 25 2016.

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2First Evaluation Of The Main Parameters In The Dynamics Of The Small Expendable Deployer System (SEDS) For A Tethered Satellite

By

The dynamics of the motion of the Small Expendable Deployer System (SEDS) is studied by using a simplified model in which no external forces (except the gravity gradient field) are applied on the tethered body and the tether is assumed massless. The dynamics of SEDS operation is modeled as a sequence of two phases: the deployment phase and the swing phase. For the first one the velocity dependent forces are found to force the tether forward from the local vertical. When the deployment ends, Coriolis effects vanish and the swing phase begins, which is characterized by a wide free libration. The time duration as well as velocity, acceleration and tension of the tethered body are estimated for both deployment and swing phases.

“First Evaluation Of The Main Parameters In The Dynamics Of The Small Expendable Deployer System (SEDS) For A Tethered Satellite” Metadata:

  • Title: ➤  First Evaluation Of The Main Parameters In The Dynamics Of The Small Expendable Deployer System (SEDS) For A Tethered Satellite
  • Author:
  • Language: English

“First Evaluation Of The Main Parameters In The Dynamics Of The Small Expendable Deployer System (SEDS) For A Tethered Satellite” Subjects and Themes:

Edition Identifiers:

Downloads Information:

The book is available for download in "texts" format, the size of the file-s is: 4.62 Mbs, the file-s for this book were downloaded 275 times, the file-s went public at Mon Jul 26 2010.

Available formats:
Abbyy GZ - Animated GIF - Archive BitTorrent - DjVu - DjVuTXT - Djvu XML - JPEG Thumb - Metadata - Scandata - Single Page Processed JP2 ZIP - Text PDF -

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