GALILEO
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The Galileo Energetic Particles Detector
Galileo EPD Handbook
Chapter 1. Instrument Summary
CMS Rate Channels - Post-Challenger Information
Source: Critical Design Review, December 1987
Changes to existing circuit boards:
Description of New Hardware Tasks
- Process KT detector signal
- Control high voltage converter
- Switch HVPS power by command
- Route new signals through polytwist
- Process events
- Add additional RAM to data system
- Change J'C aperture into J'B
Figure 1-23. Proposed configuration changes for new EPD CMS subsystem
Spacecraft interface
- No new wires or signals required for new configuration
- Additional load on main spacecraft 15 voltage bus
for HVPS
- EPD is on the protected spacecraft bus
- Fuse protected (redundant)
- Relay switched by protected command
- Possible EMI/EMC interaction; measured by testing at JPL SAF
Analog filter board rework
- Functional description of changes
- KT signal processed by old L and JB amps
- JB' and KB' signal into old JC' and KC' amps
- JB bias, KT bias
- Calibrator signal into TOF channel (TCAL)
- Mounted inside new TOF box
- Parts questions: none
- Functional testing results: no major problems; difficulty switching KT bias
- Known outstanding design issue: select proper K bias network
- Scope: Add 7 components, remove 15; add 7 lines, remove 11
Figure 1-24. Functional Block Diagram of Analog Filter Board
CMS analog electronics
- Basic board operation
- Functional description of changes
- KT signal processed by old JC' amps
- Discriminator input routing changed
- Mass channels defined by KT and T (not K)
- Valid event logic definitions changed
- Calibrator signal into TOF channel (TCAL)
- Component packaging: unchanged
- Parts questions: none
- Functional testing results: no major problems; more rate testing, etc., necessary
- Known outstanding design issues: TCAL signal not sent to rate logic or PHA
- Scope: Add 2 components, remove 14; add 20 lines, remove 16
Figure 1-25. CMS analog electronics chain
CMS rate logic (new version of previous design)
- Functional description of changes
- New rate channel definitions for KT x T
- Elimination of CE, CP, and JC channels
- New ID code format
- Component packaging: minor changes
- Parts questions: limited accumulator hybrids
- Functional testing results: no problems
- Known outstanding issue: calibrator mux assignments must be modified
Low voltage power converter
- Basic board operation
- Functional description of changes
- Relay (K71) to switch 15 volts for HVPS
- Old "JA00" command line used to command K71
- Filter replaces divider on "K bias board"
- 3 volt dummy loads removed - zenors added
- Component packaging: minor changes
- Parts questions: none
- Functional testing results: no problems
- Known outstanding design issues: none
- Scope: Add 10 components, remove 4; add 4 lines, remove 10
Next: CMS Rate Channels - Pre-Challenger Information
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Updated 8/23/19, Cameron Crane
QUICK FACTS
Manufacturer: The Galileo Spacecraft
was manufactured by the Jet Propulsion Laboratory,
Messerschmitt-Bölkow-Blohm, General Electric, and the
Hughes Aircraft Company.
Mission Duration: Galileo was planned to have a mission duration of around 8 years, but was kept in operation for 13 years, 11 months, and 3 days, until it was destroyed in a controlled impact with Jupiter on September 21, 2003.
Destination: Galileo's destination was Jupiter and its moons, which it orbitted for 7 years, 9 months, and 13 days.
Mission Duration: Galileo was planned to have a mission duration of around 8 years, but was kept in operation for 13 years, 11 months, and 3 days, until it was destroyed in a controlled impact with Jupiter on September 21, 2003.
Destination: Galileo's destination was Jupiter and its moons, which it orbitted for 7 years, 9 months, and 13 days.