Changeset 171 in JEM-EUSO

Timestamp:

Jun 5, 2013, 10:53:36 AM (11 years ago)

Author:

moretto

Message:

version du 4 juin avec nouveau design de la nacelle

Location:

ICRC2013/EusoBalloonDetector/trunk

Files:

• GlobalViewInstrument.pptx (modified) (previous)
• GlobalViewInstrument2.png (added)
• icrc2013-EBDet-morettodagoret.log (modified) (6 diffs)
• icrc2013-EBDet-morettodagoret.pdf (modified) (previous)
• icrc2013-EBDet-morettodagoret.synctex.gz (modified) (previous)
• icrc2013-EBDet-morettodagoret.tex (modified) (2 diffs)

ICRC2013/EusoBalloonDetector/trunk/icrc2013-EBDet-morettodagoret.log

@@ -1 @@
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- [2 <./GlobalViewInstrument.jpg> <./InstrumentTable.png>]
+ [2 <./GlobalViewInstrument2.png> <./InstrumentTable.png>]
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@@ -453 +453 @@
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@@ -481 +479 @@
 ### bottom level 
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-Output written on icrc2013-EBDet-morettodagoret.pdf (4 pages, 529222 bytes).
+Output written on icrc2013-EBDet-morettodagoret.pdf (4 pages, 476940 bytes).
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ICRC2013/EusoBalloonDetector/trunk/icrc2013-EBDet-morettodagoret.tex

@@ -82 +82 @@
  \begin{figure} 
   \centering
-  \includegraphics[width=0.4\textwidth]{GlobalViewInstrument.jpg}
+  \includegraphics[width=0.48\textwidth]{GlobalViewInstrument2.png}
   \caption{EUSO-Balloon Instrument Overview.}
   \label{fig:globalview}
@@ -104 +104 @@
 The mechanics of the instrument is made of Fibrelam\textregistered \ panels, arranged together through fiberglass sections.
 The instrument is coated by an insulating cover to protect the components from fast temperature changes during balloon ascent and descent.
-Special watertight valves, inserted in the optical bench, are used to enable pressure equilibrium with the external environment. Wherever the after-flight landing location occurs, the instrument must be recovered  with the smallest damages. The bottom part is therefore equipped with crash-pads, which absorb strong deceleration (up to 15 g) when landing on ground. A baffle with special holes in the optical bench are used as a piston-effect to damp the shock for a fall over water.
+Special watertight valves, inserted in the optical bench, are used to enable pressure equilibrium with the external environment. Wherever the after-flight landing location occurs, the instrument must be recovered  with the smallest damages. The bottom part is therefore equipped with crash rings, which absorb strong deceleration (up to 15 g) when landing on ground. A baffle with special holes in the optical bench are used as a piston-effect to damp the shock for a fall over water.
 The instrument booth, a totally watertight sealed box, consists of a central aluminium plate on which the various electronic boxes are fixed. One of its side is the third lens. The opposite side is an aluminium radiator used to dissipate the heat generated by the electronics. The instrument is surrounded by buoys to avoid sinking in case of splashdown and to raise straight up the instrument booth above the water level.