CASSINI
Cassini MIMI Investigation at Fundamental Technologies
Historical MIMI Memos and Notes
MIMI/LEMMS 180 Degree End (Obverse)
Passband Summary
| CHANNEL |
ELECTRONS MeV |
PROTONS MeV |
ALPHAS MeV/Nuc. |
CARBON MeV/Nuc. |
OXYGEN MeV/Nuc. |
IRON MeV/Nuc. |
| P1 | X | X | X | X | X | X |
| P2 | X | X | X | X | X | X |
| P3 | X | X | X | X | X | X |
| P4 | X | X | X | X | X | X |
| P5 | X | X | X | X | X | X |
| P6 | X | X | X | X | X | X |
| P7 | X | 39.0-44.9 | 55.5-153. | X | X | X |
| P8 | X | 48.0-71.0 | 154. 501. | X | X | X |
| P9 | X | 71.0-169 | >501. | X | X | X |
| E1 | X | X | X | X | X | X |
| E2 | X | X | X | X | X | X |
| E3 | X | X | X | X | X | X |
| E4 | X | X | X | X | X | X |
| E5 | 2.951-1000. | 429-495 | X | X | X | X |
| E6 | X | >495 | X | X | X | X |
| E7 | 2.567-1000. | 105-369 | X | X | X | X |
| H1 | X | X | X | X | 2.95-3.40 | 3.164-3.40 |
| H2 | X | X | X | 119-205 | 222-552 | X |
| H3 | X | X | 39.0-48.1 | 119-696 | >222 | X |
| H4 | X | X | 48.1-55.5 | >696 | X | X |
| H5 | X | 20.8-25.6 | 55.5-82.8 | X | X | X |
| Z1 | X | X | X | X | X | X |
| Z2 | X | X | X | X | X | X |
| Z3 | X | X | X | 73.1-119 | 90.1-222. | >157 |
| D1 | 82.5-1000. | >41-962 | >41.8 | >78.3 | >90.1 | >168 |
| D2 | 3.4-1000. | >39.0 | >39.0 | >73.1 | >90.1 | >157 |
| D3 | 2.75-1000. | >33.9 | >33.9 | >63.6 | >78.3 | >146 |
| D4 | 2.57-1000. | >31.6 | >31.6 | >59.3 | >72.1 | >137 |
| B | >3.9 | >3.9 | >7.3 | >8.4 | >11.9 |
| ABSORBER NAME | CONTACT | A | B | ABS. | D4 | D3 | D2 | D1 |
| ABS. THICKNESSES,MICRONS | 0.1 | 150.0 | 700.0 | 1000.0 | 700.0 | 1400.0 | 700.0 | 150.0 |
| ABSORBER MATERIAL | ALUM. | SILICON | SILICON | GOLD | SILICON | SILICON | SILICON | SILICON |
| THICKNESS VAR'N,MICRONS | 0.0 | 50.0 | 10.0 | 10.0 | 10.0 | 10.0 | 10.0 | 10.0 |
| CONICAL HALF ANGLE,DEGREES | 7.5 | 7.5 | 7.5 | 15.0 | 15.0 | 15.0 | 15.0 | 15.0 |
| DETECTOR NOISE,MEV | 0.010 | 0.010 | 0.010 | 0.007 | 0.020 | |||
| ELECTRONIC NOISE,MEV | 0.006 | 0.010 | ||||||
| NUMBER OF THRESHOLDS SET | 0.0 | 9.0 | 5.0 | 0.0 | 5.0 | 5.0 | 6.0 | 7.0 |
| THRESHOLD LEVEL NO.MEV 1 | 0.012 | 0.100 | 0.100 | 0.050 | 0.050 | 0.075 | ||
| THRESHOLD LEVEL NO.MEV 2 | 0.030 | 0.400 | 0.400 | 0.400 | 0.700 | 0.200 | ||
| THRESHOLD LEVEL NO.MEV 3 | 0.050 | 1.000 | 1.000 | 3.000 | 3.000 | 0.400 | ||
| THRESHOLD LEVEL NO.MEV 4 | 0.100 | 4.000 | 2.800 | 6.000 | 6.000 | 0.760 | ||
| THRESHOLD LEVEL NO.MEV 5 | 0.250 | 13.000 | 5.000 | 16.000 | 12.000 | 1.600 | ||
| THRESHOLD LEVEL NO.MEV 6 | 0.500 | 4 | 5.000 | |||||
| THRESHOLD LEVEL NO.MEV 7 | 0.800 | 18.000 | ||||||
| THRESHOLD LEVEL NO.MEV 8 | 1.600 | |||||||
| THRESHOLD LEVEL NO.MEV 9 | 5.000 | |||||||
| AVG PROJECTED DEPTH (MIC) | 0.2 | 150.6 | 703.0 | 1017.3 | 712.1 | 1424.3 | 712.1 | 152.6 |
| EST.RMS VAR'N.PROJ.DEPTH,MIC | 0.0 | 0.6 | 3.0 | 17.6 | 12.3 | 24.7 | 12.3 | 2.6 |
| NET RMS THICKNESS VARN.(MIC) | 0.0 | 50.0 | 10.4 | 20.3 | 15.9 | 26.6 | 15.9 | 10.3 |
| LOWER LIMIT THICKNESS(MIC) | 0.1 | 100.6 | 692.6 | 997.1 | 696.2 | 1397.6 | 696.2 | 142.3 |
| UPPER LIMIT THICKNESS(MIC) | 0.2 | 200.6 | 713.5 | 1037.6 | 728.0 | 1450.9 | 728.0 | 162.9 |
| CHANNEL NAME, LOGIC |
LOGIC MAP ABSORBER,LEVEL, (1=TRUE), (-1=FALSE) |
| P7 D21(D25)D33(D35) | 7 2 1 7 5-1 6 4 1 6 5-1 |
| P8 D12(D15)D22(D23)D33 | 8 2 1 8 5-1 7 2 1 7 3-1 6 3 1 |
| P9 D22(D23)D32(D33) | 7 2 1 7 3-1 6 2 1 6 3-1 |
| E5 D21(D22)D32(D33) | 3 1 1 3 2-1 6 2 1 6 3-1 |
| E6 D32(D33)D41(D42)(B1) | 6 2 1 6 3-1 5 1 1 5 2-1 3 1-1 |
| E7 D41(D42)B1(B2) | 5 1 1 5 2-1 3 1 1 3 2-1 |
| G1 (D21)D31(D32)(D41) | 7 1-1 6 1 1 6 2-1 5 1-1 |
| H2 D16(D17)D21(D26) | 8 6 1 8 7-1 7 1 1 7 6-1 |
| H3 D25(D26)D32 | 7 5 1 7 6-1 6 2 1 |
| H4 D23(D25)D35 | 7 3 1 7 5-1 6 5 1 |
| H5 D22D34(D35)D45 | 7 2 1 6 4 1 6 5-1 5 5 1 |
| Z3 D26D32 | 7 6 1 6 2 1 |
| D1 D11 | 8 1 1 |
| D2 D21 | 7 1 1 |
| D3 D31 | 6 1 1 |
| D4 D41 | 5 1 1 |
| B B1 | 3 1 1 |
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Updated 8/8/19, Cameron Crane
QUICK FACTS
Manufacturer: The Cassini spacecraft
was manufactured by NASA's Jet Propulsion Laboratory,
and the Huygens Probe was manufactured by Thales Alenia
Space.
Mission Duration: The Cassini-Huygens mission launched on October 15 1997, and ended on September 15 2017.
Destination: Cassini's destination was Saturn and its moons. The destination of the Huygens Probe's was Saturn's moon Titan.
Orbit: Cassini orbited Saturn for 13 years before diving between its rings and colliding with the planet on September 15th, 2017.
Mission Duration: The Cassini-Huygens mission launched on October 15 1997, and ended on September 15 2017.
Destination: Cassini's destination was Saturn and its moons. The destination of the Huygens Probe's was Saturn's moon Titan.
Orbit: Cassini orbited Saturn for 13 years before diving between its rings and colliding with the planet on September 15th, 2017.