Failures/Galileo (Jupiter orbiter)
Galileo high-gain antenna failed to fully open
galileo-hga-1991What happened
When commanded open in April 1991, the umbrella-like main antenna opened only partly. JPL analysis concluded that 4 of its 18 ribs were stuck.
Why
High friction between a few rib pins and their sockets. The bonded MoS2 dry lubricant on those pins was most likely lost before launch, and the bare titanium pins galled (seized) against the Inconel sockets. The deployment motor then bent the pins during the first attempt.
| Explanations in the sources | Source |
|---|---|
| Lubricant shaken or worn off during pre-launch transport (cross-country truck trips). | Galileo spacecraft description (NASA Planetary Data System catalog file); The Galileo trials (Spaceflight Now, 2003) |
| Lubricant degraded during the long storage caused by launch delays.Unconfirmed; from a secondary source. | Galileo's antenna problem (The Logbook) |
Evidence
| Measurement | Value | Source |
|---|---|---|
| friction coefficient, lubricated Ti-6Al-4V on Inconel 718, in vacuum | 0.04 | Properties Data for Opening the Galileo's Partially Unfurled Main Antenna |
| friction coefficient, lubricated Ti-6Al-4V on Inconel 718, in air | 0.13 | Properties Data for Opening the Galileo's Partially Unfurled Main Antenna |
| dry-film lubricant endurance life, vacuum vs air | about 1000 times longer in vacuum | Properties Data for Opening the Galileo's Partially Unfurled Main Antenna |
| friction coefficient, unlubricated Ti-6Al-4V on Inconel 718, in vacuum (galling) | 1.2 (1.45 when wear debris clogged the interface) | Properties Data for Opening the Galileo's Partially Unfurled Main Antenna |
| friction coefficient, lubricated pin run first in humid air then in vacuum (galling) | 0.32 in humid air, 1.4 in vacuum | Properties Data for Opening the Galileo's Partially Unfurled Main Antenna |
Consequence
The mission ran on the small low-gain antenna. Without changes it would have sent only 8 to 16 bits per second from Jupiter. Software changes on the spacecraft and on the ground raised this to as much as 160 bits per second, and lossy compression shrank some image and plasma-wave data to as little as 1/80 of its original size.
Lessons
Space Mushroom's reading of the sources, not quotes from them.
- MoS2 dry-film lubricants wear far faster in air than in vacuum, so handling, transport and ground tests in air can use up lubricant life before launch.
- Once a dry-film lubricant is gone, titanium sliding on nickel alloy in vacuum can gall and seize, with friction above 1.
- Check lubricant condition after every transport and before final integration.
Full record
spore: failure
id: galileo-hga-1991
spore_version: 0.1
status: measured
org: nasa
title: Galileo high-gain antenna failed to fully open
mission: Galileo (Jupiter orbiter), launched October 1989 from Space Shuttle Atlantis
date: 1991-04
component: high-gain antenna rib alignment (standoff) pins
materials:
- {role: pin, name: Ti-6Al-4V titanium alloy, treatment: Tiodize, category: metals, type: titanium}
- {role: lubricant, name: Tiolube 460 bonded dry film, active_ingredient: molybdenum disulfide (MoS2), thickness_um: 25, category: tribology, type: dry-lubricants}
- {role: counterface, name: Inconel 718 nickel superalloy, category: metals, type: nickel-superalloys}
environment: [vacuum, deep space]
tags:
environments: [deep-space]
stresses: [vacuum-and-outgassing, galling-and-cold-welding]
applications: [mechanisms]
symptom: >
When commanded open in April 1991, the umbrella-like main antenna opened only
partly. JPL analysis concluded that 4 of its 18 ribs were stuck.
root_cause:
summary: >
High friction between a few rib pins and their sockets. The bonded MoS2 dry
lubricant on those pins was most likely lost before launch, and the bare
titanium pins galled (seized) against the Inconel sockets. The deployment
motor then bent the pins during the first attempt.
confidence: likely
competing_explanations:
- explanation: Lubricant shaken or worn off during pre-launch transport (cross-country truck trips).
sources: [pds-galileo, spaceflightnow-2003]
- explanation: Lubricant degraded during the long storage caused by launch delays.
sources: [logbook]
note: Unconfirmed; from a secondary source.
evidence:
- measurement: friction coefficient, lubricated Ti-6Al-4V on Inconel 718, in vacuum
value: 0.04
source: nasa-tm-105355
- measurement: friction coefficient, lubricated Ti-6Al-4V on Inconel 718, in air
value: 0.13
source: nasa-tm-105355
- measurement: dry-film lubricant endurance life, vacuum vs air
value: about 1000 times longer in vacuum
source: nasa-tm-105355
- measurement: friction coefficient, unlubricated Ti-6Al-4V on Inconel 718, in vacuum (galling)
value: 1.2 (1.45 when wear debris clogged the interface)
source: nasa-tm-105355
- measurement: friction coefficient, lubricated pin run first in humid air then in vacuum (galling)
value: 0.32 in humid air, 1.4 in vacuum
source: nasa-tm-105355
consequence: >
The mission ran on the small low-gain antenna. Without changes it would have
sent only 8 to 16 bits per second from Jupiter. Software changes on the
spacecraft and on the ground raised this to as much as 160 bits per second, and
lossy compression shrank some image and plasma-wave data to as little as 1/80
of its original size.
lessons:
# Space Mushroom's reading of the sources, not a quote from them.
- MoS2 dry-film lubricants wear far faster in air than in vacuum, so handling, transport and ground tests in air can use up lubricant life before launch.
- Once a dry-film lubricant is gone, titanium sliding on nickel alloy in vacuum can gall and seize, with friction above 1.
- Check lubricant condition after every transport and before final integration.
sources:
- key: nasa-tm-105355
title: Properties Data for Opening the Galileo's Partially Unfurled Main Antenna
id: NASA TM-105355 (Miyoshi and Pepper, NASA Lewis Research Center, February 1992)
url: https://ntrs.nasa.gov/citations/19920011418
where: Summary and Introduction
- key: pds-galileo
title: Galileo spacecraft description (NASA Planetary Data System catalog file)
url: https://pds-ppi.igpp.ucla.edu/volume/GOMW_5005/EXTRAS/CATALOG_FILES/GO_SPACECRAFT_DESC_INST.TXT
where: High-gain antenna and low-gain antenna sections
- key: spaceflightnow-2003
title: The Galileo trials (Spaceflight Now, 2003)
url: https://spaceflightnow.com/galileo/030921galileohistory.html
- key: logbook
title: Galileo's antenna problem (The Logbook)
url: https://www.thelogbook.com/galileos-antenna-problem/
license: CC-BY-4.0
Sources
- Properties Data for Opening the Galileo's Partially Unfurled Main Antenna. NASA TM-105355 (Miyoshi and Pepper, NASA Lewis Research Center, February 1992), Summary and Introduction.
- Galileo spacecraft description (NASA Planetary Data System catalog file), High-gain antenna and low-gain antenna sections.
- The Galileo trials (Spaceflight Now, 2003).
- Galileo's antenna problem (The Logbook).