Astrionics

Results: 27



#Item
1Bore Hole Monitoring – Coal Seam Gas Projects Southern Queensland

Bore Hole Monitoring – Coal Seam Gas Projects Southern Queensland

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Source URL: aha.net.au

Language: English - Date: 2014-10-22 18:16:42
2Exsys Case Study Satellite Diagnostics – Anomaly Identification and Resolution Multi-Mission Advanced Ground Intelligent Control US Air Force - Space and Missile Systems Center

Exsys Case Study Satellite Diagnostics – Anomaly Identification and Resolution Multi-Mission Advanced Ground Intelligent Control US Air Force - Space and Missile Systems Center

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Source URL: www.exsys.com

Language: English - Date: 2013-10-15 23:19:39
3Chapter 5:  Spacecraft and Mission Design The spacecraft characteristics as the baseline are summarized in Table 5.1. Key items of the characteristics are described in following sections.

Chapter 5: Spacecraft and Mission Design The spacecraft characteristics as the baseline are summarized in Table 5.1. Key items of the characteristics are described in following sections.

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Source URL: hinode.nao.ac.jp

Language: English - Date: 2011-04-28 05:40:11
4Laser Telemetry from Space Joss Bland-Hawthorn Anglo-Australian Observatory, Epping, NSW, 2121 Australia Alex Harwit Transparent Networks, Santa Clara, CA 95050, USA Martin Harwit

Laser Telemetry from Space Joss Bland-Hawthorn Anglo-Australian Observatory, Epping, NSW, 2121 Australia Alex Harwit Transparent Networks, Santa Clara, CA 95050, USA Martin Harwit

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Source URL: www.physics.usyd.edu.au

Language: English - Date: 2002-05-22 21:40:26
54-3 Telemetry and Command Processing System for Experiments OHASHI Hajime Two telemetry and command processing systems are being prepared as part of the ground facilities by CRL to monitor and control CRL’s onboard equ

4-3 Telemetry and Command Processing System for Experiments OHASHI Hajime Two telemetry and command processing systems are being prepared as part of the ground facilities by CRL to monitor and control CRL’s onboard equ

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Source URL: www.nict.go.jp

Language: English - Date: 2004-11-12 13:24:04
6Horizon Sensing Attitude Stabilisation: A VMC Autopilot Presented to the 18th International UAV Systems Conference, Bristol, UK, 2003 B. Taylor C. Bil S. Watkins School of Aerospace, Mechanical and Manufacturing Engineer

Horizon Sensing Attitude Stabilisation: A VMC Autopilot Presented to the 18th International UAV Systems Conference, Bristol, UK, 2003 B. Taylor C. Bil S. Watkins School of Aerospace, Mechanical and Manufacturing Engineer

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Source URL: www.eganfamily.id.au

Language: English - Date: 2010-05-19 21:40:15
7Earth Calling… Overview: A hands-on activity exploring spacecraft radio communication concepts, including the speed of light and the time-delay for signals sent to and from spacecraft.  Target Grade Level: 6-8

Earth Calling… Overview: A hands-on activity exploring spacecraft radio communication concepts, including the speed of light and the time-delay for signals sent to and from spacecraft. Target Grade Level: 6-8

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Source URL: pluto.jhuapl.edu

Language: English - Date: 2014-12-15 16:33:09
8Earth Calling… Overview: A hands-on activity exploring spacecraft radio communication concepts, including the speed of light and the time-delay for signals sent to and from spacecraft.  Target Grade Level: 6-8

Earth Calling… Overview: A hands-on activity exploring spacecraft radio communication concepts, including the speed of light and the time-delay for signals sent to and from spacecraft. Target Grade Level: 6-8

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Source URL: pluto.jhuapl.edu

Language: English - Date: 2014-12-11 12:29:44
9[removed]Command Subsystem. The IUE command subsystem consists of redundant command decoders and a command relay unit (CRU), as is shown in the figure 5-18.The CRU contains circuit redundancy up to the individual relay a

[removed]Command Subsystem. The IUE command subsystem consists of redundant command decoders and a command relay unit (CRU), as is shown in the figure 5-18.The CRU contains circuit redundancy up to the individual relay a

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Source URL: godot.u-strasbg.fr

Language: English - Date: 2000-12-05 06:33:19
103  2. General spacecraft description. The IUE spacecraft is shown in mission orbit configuration and in an exploded view in figures 2-1 and 2-2 respectively.

3 2. General spacecraft description. The IUE spacecraft is shown in mission orbit configuration and in an exploded view in figures 2-1 and 2-2 respectively.

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Source URL: godot.u-strasbg.fr

Language: English - Date: 2000-12-05 06:33:19