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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

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