Observations of Charge Sign Dependence in Solar Modulation

1. Observations of Charge Sign Dependence in Solar Modulation Kiruna 2009 LEE Low Energy Electrons P.I.C. November 13, 2008 • John Clem and Paul Evenson

2. Overview • I will discuss LEE science and the interface of LEE to the MIP • John Clem will discuss AESOP science and all other aspects of the campaign

3. LEE Scientific Objectives • Keep the standard candle of electron observations burning • Provide an intercalibration with PAMELA • Search for the origin of the turn up in the low energy electron spectrum

4. For Decades the Cosmic Ray Electron “Standard Candle” Has Been LEE Magnetic Polarity • Time profile of helium and electron observations at a rigidity of 1.2 GV

5. LEE Data Were Used to Correct and Validate the Response of the Kiel Electron Telescope (KET) on Ulysses Correlation of 1.2 GeV and 2.5GeV Electron Fluxes observed at Earth by LEE and ICE with uncorrected Ulysses 1.2 GeV and 2.5GeV electron channel. Solid lines are linear least squares fits to the data. The relative normalization of the LEE and ICE data sets was also adjusted to minimize the chi square of the linear fits.

6. Radial Gradient (1 To 5 AU ) of Cosmic Ray Electrons at 1.2 and 2.5 GV • Prior studies: McDonald et al 1997, Fujii and McDonald 1997, Heber et. al. 2002 • Our analysis uses LEE, ICE, and Ulysses data. • Squares: Gradients of positive charged particles. • Circles: Gradients of negative charged particles. • Red: 1.2 GV • Green: 1.7 GV • Black 2.5 GV

7. Electron Latitude Gradient • Fractional deviation between the observed LEE fluxes and KET fluxes of 1.2GV electrons as a function of helio-latitude of the Ulysses spacecraft. • Latitude gradient appears after the solar polarity reversal

8. Electron/Helium Flux Ratio (At 1.2 GV) as a Function of Current Sheet Tilt Angle

9. Investigation Of The Electron Spectrum At Low Energy • High altitude is critical to the search for the origin of the mysterious turn up in the low energy electron spectrum 20 MeV

10. In August of 2002 LEE flew on a 60mcf balloon reaching float at 161kft (0.9 mbar). The high altitude provided a low background environment allowing measurements of primary electrons with energies as low as 20MeV.

11. The LEE Payload • LEE detects electrons with • Plastic scintillators T1, T3 and G (anticoincidence) • Gas Cherenkov detector T2. • It measures the electron energy with • Cesium iodide (T4) calorimeter • Lead glass (T5) calorimeter • Scintillator T6 assists in particle identification and energy determination by counting the number of particles that escape the calorimeter. 25

12. LEE Flight Requirements • Desired • Altitude 135 kft • Duration 60 hrs • Minimum • Altitude 120 kft • Duration 36 hrs • Flight Profile • Remain north of 0.5 GV geomagnetic cutoff • Altitude excursions are helpful

13. LEE Power (Battery): Heaters Off: 20watts Heaters On: 90watts (80-hrs of 32V-battery weigh roughly the same as a solar power system, therefore LEE does not solar power to achieve desired goals.) LEE Telemetry: COMM1 Connection to MIP Downlink: Iridium, LOS Uplink: Iridium, LOS Two Discrete Lines (Power On/Off) High Rate Umbilical for Final Checkout

14. LEE Work Space • 20 x 20 ft work space • ½ ton overhead lift • 5 x 115V power outlets (50 amp) • 60hz converters for running motors • Phone line • Reliable internet service to OCC (Palestine)

15. LEE Payload Status • Tested with MIP in August of 2007 • We expect to be in Palestine early February and ready for compatibility hanging mid-month • We will require 7 days of preparation time in Kiruna before declaring flight-ready

16. Issue • Our GSE can easily be modified to deal with COMM1 and COMM2 on the MIP • There is only one port on the instrument, which we plan to connect to COMM1 • Possible input “or” and output “fanout” would have to be in CSBF package