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#91 |
Not funny anymore
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How much dV do you plan with? Depending on how we deploy it, we need different maneuver budgets for it.
When we release it during Earth-Mars-Transfer, we only need a little bit of dV for correcting impact site. If we release it from Mars Orbit, we need much more dV for getting a steep enough reentry angle. |
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#93 |
Spring of Life!
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Looks good! I think she will go boom quite adequately.
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#94 |
Not funny anymore
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![]() Last edited by Urwumpe; 01-09-2012 at 01:22 AM. Reason: Proper translation of German proverb |
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#95 |
Moderator
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It has around 500 m/s dV with the current code, using solid motors for deorbit
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#96 |
Wanderer
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#97 |
Moderator
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somoeone might want to inspect impact crater after impactor hits mars surface:
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#98 |
Acolyte of the Probe
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Good idea! no work needed to expose multiple layers of regolith. If we kick it out while in transit, then give it a slight nudge, and have it target near the planned LZ, it's a short hop away. However, we would need to have the sensors emplaced beforehand.
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#99 |
Moderator
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Short before reentry
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#100 |
JapanAXA!
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#101 |
Not funny anymore
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Still, we don't want it to impact near the LZ, we want it at the right distance to get seismic data... 135° great circle distance to the seismometer array should do it. Accuracy during landing is needed for another reason: It reduces the errors in the seismic data. We can reconstruct the impact zone from the seismic data, but we get more inaccuracy, the worse the impact accuracy is to start with.if we can monitor the impact visually from space with a telescope, we should be able to get much better impact data, but I can't tell the visibility during this work-load heavy phase. Maybe we should coordinate the impact with a previously deployed Mars satellite. Last edited by Urwumpe; 01-09-2012 at 10:01 PM. |
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Thanked by: |
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#102 |
JapanAXA!
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#104 |
Not funny anymore
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![]() (BTW: In reality it is more deep than high, the crater rims are too steep and too high compared to the depth of the crater) |
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#105 |
Moderator
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It's around 60 meter wide
Too big? |
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ofmm mission planning |
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