Differences between revisions 3 and 5 (spanning 2 versions)

mur.sat Wiki

This wiki is powered by MoinMoin.

Project

mur.at will launch a setellite. Interorbital Systems offers its TubeSat personal satellite kit for aprox. USD 8,600 (launch inclusive). The satellite will occupy a LEO for a couple of weeks before burning in the athmosphere on reentry.

LEO

Low Earth Orbit (see e.g. Wikipedia for more).

3~4 min per day visibility from Graz/Austria

website layout example links

http://n2yo.com/

usage ideas

as many sensors as possible ()
- orientation sensor (magnetic field)
- Inertialsensor (movement)
- Photoresistor ???
- WebCam without IR filter!
- radio scanner (what do you hear in space?)
  - drag an antenna? antenna pole for gradient stabilasation (is this term correct?); exactly orthogonal to receiving direction ...
place a high power LED on satellite that blinks when orientation towards earth fits so - using long term exposure - one could get a pattern.
sending/receiving data via website (store and forward) should/will be possible

-  ⇤ ← Revision 3 as of 2010-07-23 17:16:26 → 
  Size: 1185
  Editor: xro
  Comment:
+   ← Revision 5 as of 2010-07-28 14:27:13 → ⇥
  Size: 1305
  Editor: JogiHofmueller
  Comment:
-Deletions are marked like this.
+Additions are marked like this.
 Line 9:
-= Projekt =
mur.at will einen Satelliten ins All schießen. das wird um rund 8600 Dollar vom Unternehmen Tubesat angeboten. Das Teil befindet sich dann ein paar Wochen im LEO bevor es in der Atmosphäre verbrennt. Durch Verwendung einer Attitude Control fliegt das Teil natürlich länger.
+= Project =
-Line 12:
+Line 11:
-=== LEO Orbit ===
 3~4 min / Tag bei uns
+mur.at will launch a setellite.  [[http://interorbital.com|Interorbital Systems]] offers its [[http://interorbital.com/TubeSat_1.htm|TubeSat]] personal satellite kit for aprox. USD 8,600 (launch inclusive).  The satellite will occupy a LEO for a couple of weeks before burning in the athmosphere on reentry.
-Line 15:
+Line 13:
-=== website layout beispiel links ===
+=== LEO ===

Low Earth Orbit (see e.g. [[http://en.wikipedia.org/wiki/Low_Earth_orbit|Wikipedia]] for more).

3~4 min per day visibility from Graz/Austria

=== website layout example links ===
-Line 18:
+Line 23:
-=== VerwendungsIdeen: ===
 * mög. viele Sensoren (Weltraum am Boden erlebbar machen)
 * Orientierungssensor (Magnetfeld)
 * Inertialsensor (Bewegung)
 * Photoresistor ???
 * WebCam ohne IR Filter !
 * RadioScanner (Was hört man im Weltraum von uns ? 
     (Antenne hinten nachziehen ? bzw Antennenstange zur Gradientenstabilisierung, dann aber genau orthogonal zur Empfangsrichtung :-( )
 * SuperLED am Sat, blink wenn Orientierung zur Erde passt -> Im Langzeitbelichtungsfoto von Erde aus Muster sichtbar.
  (lichtstärke ? wieviel kommt an)
 * über Webseite Senden/Empfangen (Store&Forward) soll möglich sein
+=== usage ideas ===

 * as many sensors as possible ()
  * orientation sensor (magnetic field)
  * Inertialsensor (movement)
  * Photoresistor ???
  * WebCam without IR filter!
  * radio scanner (what do you hear in space?)
   * drag an antenna?  antenna pole for gradient stabilasation (is this term correct?);  exactly orthogonal to receiving direction ...
 * place a high power LED on satellite that blinks when orientation towards earth fits so - using long term exposure - one could get a pattern.
 * sending/receiving data via website (store and forward) should/will be possible