
Figure 9. PHM EM frequency and time stabilities
- Teflonization of the quartz storage Bulb
- Hydrogen beam assembly
- Getters assembly
- Tuning of the microwave cavity
- H2 purifier assembly
- Magnetic shield assembly
- State selector assembly
- Hydrogen supply and dissociator
Fig. 10 shows the atomic response of the PHM physics
package, measured with 15Hz span exhibiting atomic signal
gain of 3.8dB and atomic line width of 2 Hz.
The new design of the physics package has been also
focussed on parts count reduction. Less than one half
individual parts has been used in the new design compared to
the EM model.
For the electronics package and the whole instrument:
- Reduction of PHM volume and footprint
- Improvement of TM/TC interface
- Ground operability at ambient pressure
- Redesign of hydrogen dissociator
- Improvement of thermal and pressure controls
- Redesign of PHM and Purifier supply

Figure 10. PHM atomic signal measured in FM1

Figure 11. Technological models with/without cover
Two technological models (Fig. 11), a Structural Model
and an EQM were built for these objectives and to qualify
the new upgraded design. In addition, four EQMs for life
demonstration are being manufactured and will be submitted
to prolonged testing. In the frame of GSTB-V2, which is
presently being tested at P/L level, one PFM (Fig. 12) has
completed the proto-qualification testing and has been
delivered. One spare FM will be delivered by the end of
2005. Table II shows the achieved performance of
PHM/PFM for GSTBV2. Significant improvement has been
achieved by a better silver coating process and surface
polishing of the magnetron cavity (Fig 13). Fig. 14 is
showing the performances improvements of the physics
package of FM1 model before its integration, obtained by the
quality factor improvement.

Figure 12. Picture of PHM PFM
TABLE II. PHM FOR GSTB-V2 PERFORMANCE ACHIEVED
| Parameter | Measurement |
| Frequency stability | < 1*10-14 @ 10’000 sec |
| Flicker floor | < 7*10-15 |
| Thermal sensitivity | < 3*10-14 /°C |
| Magnetic sensitivity | < 4*10-14 / Gauss |
| Mass and volume | 18 kg and 28 liter |

Figure 13. PHM magnetron cavity

Figure 14. PHM performance improvement
PHM Lifetime
The PHM is being sized to guarantee 12 years of orbit
life plus 1 year of ground storage, as well as the complete
AIT program. The operational life is mainly limited by
capacities of the hydrogen container (for H2 supply), bulk
getters (for H2 sorption), ion pump (for pumping
ungetterable background gases) and the total dose of ionising
radiation. The lifetime is assessed by analysis and tests of
subassemblies.
Fig. 15 shows the H2 consumption test made in June
2005, which indicates the consumption of 1.53 bar*l/year at
nominal flux, by measuring the pressure decay in the known
volume of the high pressure pipeline. Taking account of the
margin from the real consumption and the retrievable H2
amount in the fixed pressure of the metal hydride, the H2
container with the capacity of 30 bar*l is sufficient for the
operational life time.
A novel custom built getter pump is developed for the
PHM. The getter material provides high sorption capability
and mechanical stability. The H2 sorption test on the getter
cartridge was performed in Sep 2003. Fig. 16 shows several
cycles of the H2 filling and pumping during the test. It has
demonstrated that the getter pump is capable of sorbing the
required amount of H2 of 20 bar*l without embrittlement and
the base pressure after the sorption was in the low 10-7 mbar
range with only the getter cartridge pumping.
For the ion pump, the operating life at 5*10-6mbar is
specified 8000 hours, corresponding to 400'000 hours (45
years) at the nominal high vacuum of 10-7 mbar. Moreover,
accelerated lifetime tests of the pump in a gas composition as
close to the PHM situation as possible will be performed to
assure the pump life.
The total dose of ionising radiation over the mission
lifetime on board of the Galileo Spacecraft was analysed on
the PHM physics package and electronics package,
respectively by the approach of ‘sector’. The radiation test
will be performed.

Figure 15. H2 consumption test

Figure 16. H2 sorption test
In order to gain more field data on the reliability and
lifetime of PP subassemblies four EQMs will be produced
dedicated to the lifetime. The objective of the lifetime test is
to monitor, during the scheduled two years, the critical
parameters drift or degradation in order to predict the
lifetime of the instrument and identify possible correction
areas.
III. CONCLUSIONS
Table III summarizes the Galileo clocks status up to now.
Both clocks are subjected to electrical (functional, thermal
vacuum, EMC, etc.), as well as, mechanical tests (shock and
vibrations). Nine flight models are being produced for
GSTB-V2, which will provide the first flight opportunity for
Galileo clocks qualification. With more than 10 years of
efforts, two clock technologies for Galileo are qualified.
Those clocks use reliable and mature technologies leaving
room from further improvements in term of mass &
performances.
TABLE III. GALILEO CLOCKS STATUS
| Steps | RAFS | PHM |
| BB | Completed in 1995 | BB activity and EM design started in 2000 |
| EM | Completed in 2000 | Completed in Q1/2003 (under life test since June 2003) |
| EQM | 5 models built and under lifetime tests | 4 models available in 2006 for lifetime tests |
| QM | 1 model (RAFS1) fully qualified Rad. test Q1/2003 | 1 model |
| EQM for GSTB-V2 | 1 model delivered in August 2004 | 1 model completed in February 2005 |
| FM for GSTB-V2 | 6 models (4 delivered, 2 by Q3 /2005) | 1 model delivered, 1 model by Q4 /2005 as spare. |
REFERENCES
- A. Jeanmaire, P. Rochat, F. Emma, “Rubidium atomic clock for
Galileo,” 31st Precise Time and Time Interval (PTTI) Meeting, 07-
09 December, 1999, California (USA), pp. 627-636.
- F. Droz, P. Rochat, G. Barmaverain, M. Brunet, J. Delporte, J.
Dutrey, F. Emma, T. Pike, and U. Schmidt, “On-Board Galileo
RAFS, current status and Performances,” 2003 IEEE International
Frequency Control Symposium Jointly with the 17th European
Frequency and Time Forum, 05-08 May, 2003, Tampa (USA), pp.
105-108.
- P. Berthoud, I. Pavlenko, Q. Wang, and H. Schweda, “The
engineering model of the space passive hydrogen maser for the
European global navigation satellite system GalileoSat,” 2003 IEEE
International Frequency Control Symposium Jointly with the 17th
European Frequency and Time Forum, 05-08 May, 2003, Tampa
(USA), pp. 90-94.
- L. Mattioni, M. Belloni, P. Berthoud, I. Pavlenko, H. Schweda, Q.
Wang, P. Rochat, F. Droz, P. Mosset, and H. Ruedin, “The
development of a passive hydrogen maser clock for Galileo
navigation system,” 34th Precise Time and Time Interval (PTTI)
Meeting, 03-05 December, 2002, Reston (USA), pp. 161-170.