ULYSSES In Space

 

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ULYSSES

Ulysses HISCALE Data Analysis Handbook

 

Chapter 4: Instrument Details

 

4.4 Passband Data and Calculated Responses

 

Table 4.11 Proton and electron passbands

 

    PROTON RESPONSE ELECTRON RESPONSE
Detector Channel Low Threshold
(MeV)		 Hi Threshold
(MeV)		 Low Threshold
(MeV)		 Hi Threshold
(MeV)
LEFS60 El'(FP1') 0.362 0.375 0.042 0.065
  E2'(FP2') 0.375 0.412 0.064 0.112
  E3'(FP3') 0.412 0.460 0.112 0.178
  E4(FP4') 0.460 0.546 0.178 0.290
  FP5' 0.546 0.761    
  FP6' 0.761 1.223    
  FP7' 1.223 4.974    
LEFS150 E1(FP1) 0.363 0.372 0.040 0.065
  E2(FP2) 0.372 0.409 0.060 0.107
  E3(FP3) 0.409 0.457 0.107 0.170
  E4(FP4) 0.457 0.540 0.170 0.280
  FP5 0.540 0.765    
  FP6 0.765 1.223    
  FP7 1.223 4.942    

 

Table 4.12 LEFS detector passbands for selected ion species

 

 

 

Table 4.13 LEMS proton and ion passband summary

 

 

Notes:
1. Passband energies are in units of MeV/nucleon.
2. Passband energies in italics are extrapolated from those for neighboring species.
3. Passbands shown as <0.012 MeV/Nuc are not computer from range table here.

 

 

Table 4.14 WART passband

 

 

 

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Updated 8/8/19, Cameron Crane

QUICK FACTS

Manufacturer: ESA provided the Ulysses spacecraft, NASA provided the power supply, and various others provided its instruments.

Mission End Date: June 30, 2009

Destination: The inner heliosphere of the sun away from the ecliptic plane

Orbit:  Elliptical orbit transversing the polar regions of the sun outside of the ecliptic plane