MISSION PLAN - PDS Small Bodies Node
MISSION PLAN - PDS Small Bodies Node
MISSION PLAN - PDS Small Bodies Node
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Solar flare contribution is given as the flux at 1 AU with a required 1/r 2 to 1/r 2.5 scaling<br />
factor for other distances from the sun. The galactic cosmic ray (GCR) contribution is<br />
independent of the spacecraft location.<br />
Probability of Large Solar Events: The probability of encountering a 90% to 99%<br />
magnitude solar flare, particularly during the comet flyby, is of interest for the spacecraft<br />
design team. The probabilities are estimated by D.R. Croley (JPL IOM 5052-96-304)<br />
using the model developed by Feynman et al. at JPL. The predicted mean times between<br />
flares of 90%, 95% and 99% magnitude are given in Table 2.3-6. The table also gives the<br />
derived probability of seeing these flares during the 12 hour period around the flyby.<br />
Table 2.3-6 Probability of Large Solar Flares<br />
Flare Magnitude >90% >95% >99%<br />
Mean time (*solar- max years) ~1.4 ~2.8 ~16.9<br />
Probability of occurrence during the<br />
~1E-3 ~5E-4 ~8E-5<br />
12-hrs of the flyby<br />
*Solar-max years=~7 years of ~11 year solar cycle. All of the 7-year STARDUST mission is in the solarmax<br />
years according to the model.<br />
8<br />
10<br />
flare, no shielding<br />
6<br />
10<br />
4<br />
10<br />
2<br />
10<br />
250 mil<br />
36 mil<br />
60 mil<br />
100 mil<br />
0<br />
10<br />
Heavy -Ion Peak Flux (/cm 2/day)<br />
(Omni-Directional)<br />
-2<br />
10<br />
-4<br />
10<br />
-6<br />
10<br />
-8<br />
10<br />
GCR 25 mil<br />
GCR 500 mil<br />
1000 mil<br />
500 mil<br />
-10<br />
10<br />
1 10 100<br />
LET (MeV-cm 2/mg)<br />
JMR 12/10/96<br />
Figure 2.3-6.a Heavy-ion Flux from a 99% Solar Flare at 1 AU and<br />
for Adams’ 90% Worst Case GCR<br />
37