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of the Sun and Interplanetary Medium in Three Dimensions" May 15-16, 1975, Goddard Space Flight Center Ulysses – famous Polar Orbiter NASA/ESA 1990-2009 No solar imagers f MHz CORE1 10 CORE1 Comparing CMEs with Radio Data 20:42 21:18 Interaction Signature CME2 CME1 CME2 CME1 1 1000 km/s 700 km/s

+36,42,48,54,60,66,72,84,96,108,120,132 MSL pressure Pa 0/2 mean sea T+36,42,48,54,60,66,72,84,96,108,120,132 Rate of convective rain kg/m 2 s 0/144 ground surface T+36,42,48,54,60,66,72,84,96,108,120,132 Rate of convective snow kg/m 2 /s 0/147 ground surface T+36,42,48,54,60,66,72,84,96,108,120,132 Rate of dynamic

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Copyright 2013 27 10 Recent Publications Arnold, T., Ivy, D. J., Harth, C. M., Vollmer, M. K., Mühle, J., Salameh, P. K., Paul Steele, L., Krummel, P. B., Wang, R. H. J., Young, D., Lunder, C. R., Hermansen, O., Rhee, T. S., Kim, J., Reimann, S., O’Doherty, S., Fraser, P. J., Simmonds, P. G., Prinn, R. G

), Huruma Estate (Softkenya, 2018)(left bottom), Maongo Juu, (Ohler, S. 2016) (Right top), Tandale Sokoni, (Misilanga, M. 2018) (Right bottom) Basic Facts about Nairobi and Dar and Informal Settlements 4 DAR ES SALAAM � � � � Population: projected to be 6 million (UN-World- Urbanisation prospects, 2018

233 1 249.4 mm - 1931 England S 245.3 223 1 219.1 mm - 1936 England E & NE 295.6 254 1 208.4 mm - 1931 England NW & Wales N 347.6 206 1 287.2 mm - 1931 Midlands 312.3 267 1 227.3 mm - 1936 East Anglia 173.8 171 3 206.9 mm - 1936 England SW & Wales S 310.8 216 1 288.1 mm - 1936 England SE & central S

="">Visibility</Param> 9. <Param name="D" units="compass">Wind Direction</Param> 10. <Param name="S" units="mph">Wind Speed</Param> 11. <Param name="U" units="">Max UV Index</Param> 12. <Param name="W" units="">Weather Type</Param> 13. <Param name="Pp" units="%">Precipitation Probability</Param> 14. </Wx

Flight Dynamics Summary • Baseline Low-Thrust Trajectory to Sun-Earth L5 using Solar-Electric Propulsion • Transfer time: ~2 years • Launch C3: ~2.2 km 2 /s 2 • DV: ~1.5 km/s • Propellant (xenon) required: ~55 kg • Optional High-Thrust Trajectories using Chemical Propulsion • Transfer time: ~2 years

and is currently designing a MEL strategy for WISER. • The Met Office is seeking to appoint a Consultant(s) with necessary international development and MEL experience to provide technical support on MEL to the WISER programme. The Consultant will work with the WISER MEL Manager and independently to provide

reflectivity and high range resolution. Observation modes which observe narrower area use shorter long pulses. Pulse short long Pulse width 1μs 32, 64,128μs Japan Meteorological Agency 3 Use of short and long pulses Minimum detectable reflectivity (Sensitivity) Most sensitive pulse 30μs 67μs 129μs