ultrastable quartz oscillator

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The Johns Hopkins University APPLIED PHYSICS LABORATORY Characteristics of the ultrastable quartz oscillator. Allan variance: 1 × 10 –13 at 10 s Magnetic susceptibility: <2 × 10 –12 /g Phase noise: –137 dBc/Hz at 1 Hz Harmonic signals: –60 dBc Aging rate: <7 × 10 –13 /day Spurious signals: –80 dBc Radiation susceptibility: <1 × 10 –11 /rad (Si) Power: 0.6 W at 25°C Temp. susceptibility: <4 × 10 –13 /°C Mass: 0.4 kg The unmatched frequency stability of The Jonhs Hopkins University Applied Physics Laboratory (JHU/APL) space- qualified ultrastable quartz oscillators has been proven in nearly 50 years of space applications. JHU/APL oscillators have a demonstrated frequency stability of 1 × 10 –13 (10 s) and a temperature coefficient of 4 × 10 –13 /°C. Since the quartz oscillator is often critical to the spacecraft mission, long- term, reliable operation of the oscillator is as important as its frequency stability. Oscillators used in the Navy Navigation Satellite System accumulated over one million hours of operation in orbit without failure. One oscillator provided continuous service for more than 21 years. Over 400 JHU/APL ultrastable oscillators have been placed in orbit on a wide variety of spacecraft beginning in 1958. The environment in which the oscillator must operate has a large influence on the ultimate performance of an oscillator. Through careful design, the effects of environmentally induced frequency changes of the oscillator output frequency have been reduced to levels approaching the noise on the output frequency, as shown in the table. One environmental effect, Ultrastable Quartz Oscillator Unmatched Reliable Performance ionizing radiation, can be a substantial problem in some orbits. To address this problem, JHU/APL began conducting research on radiation effects on quartz oscillators in the late 1960s. We have developed a design that provides effective shielding from most sources of ionizing radiation found in orbit, except high- energy protons (>100MeV), thereby mitigating this effect. The inherent stability of our ultrastable oscillator can be translated to other frequencies that are coherent to the oscillator frequency by using very low noise frequency multipliers and frequency synthesis. High-isolation, low-noise buffer amplifiers provide multiple outputs with minimum cross- coupling between ports. Performance excellence and high reliability are the primary goals for JHU/APL ultra-stable oscillators; however, 07-00963-UQO.indd 1 3/13/07 2:11:53 PM

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The Johns Hopkins University APPLIED PHYSICS LABORATORY

Characteristics of the ultrastable quartz oscillator.  Allan variance:  1 × 10–13 at 10 s    Magnetic susceptibility:  <2 × 10–12/g

  Phase noise:  –137 dBc/Hz at 1 Hz    Harmonic signals:  –60 dBc

  Aging rate:  <7 × 10–13/day    Spurious signals:  –80 dBc

  Radiation susceptibility:  <1 × 10–11/rad (Si)    Power:  0.6 W at 25°C

  Temp. susceptibility:  <4 × 10–13/°C    Mass:  0.4 kg

The  unmatched  frequency  stability  of The  Jonhs  Hopkins University  Applied  Physics  Laboratory  (JHU/APL)  space-qualified  ultrastable  quartz  oscillators  has  been  proven  in nearly 50 years of space applications. JHU/APL oscillators have a demonstrated frequency stability of 1 × 10–13 (10 s) and a temperature coefficient of 4 × 10–13/°C. Since the quartz oscillator  is  often  critical  to  the  spacecraft  mission,  long-term, reliable operation of the oscillator is as important as its frequency stability. Oscillators used in the Navy Navigation Satellite  System  accumulated  over  one  million  hours  of operation  in  orbit  without  failure.  One  oscillator  provided continuous service for more than 21 years. Over 400 JHU/APL ultrastable oscillators have been placed  in orbit on a wide variety of spacecraft beginning in 1958.

The environment in which the oscillator must operate has a large influence on the ultimate performance of an oscillator. Through careful design, the effects of environmentally induced frequency changes of  the oscillator output  frequency have been reduced to levels approaching the noise on the output frequency, as shown in the table. One environmental effect, 

Ultrastable Quartz OscillatorUnmatched Reliable Performance

ionizing radiation, can be a substantial problem in some orbits. To address this problem, JHU/APL began conducting research on radiation effects on quartz oscillators in the late 1960s. We have developed a design that provides effective shielding from most sources of ionizing radiation found in orbit, except high-energy protons (>100�MeV), thereby mitigating this effect.

The  inherent  stability  of  our  ultrastable  oscillator  can  be translated  to  other  frequencies  that  are  coherent  to  the oscillator  frequency  by  using  very  low  noise  frequency multipliers and frequency synthesis. High-isolation, low-noise buffer  amplifiers  provide  multiple outputs  with  minimum  cross-coupling between ports.

Performance  excellence and  high  reliability  are the  pr imary  goals  for JHU/APL  ultra-stable oscillators;  however, 

07-00963-UQO.indd   1 3/13/07   2:11:53 PM

Applied Physics Laboratory11100 Johns Hopkins Road

Laurel MD 20723-6099240-228-5000 / Washington443-778-5000 / Baltimore

07-00963-UQO

Matt ReinhartSection Supervisor

[email protected]

For more information, contact:

http://www.jhuapl.edu/nss

power  consumption,  mass,  and  size  also  receive  careful attention. These parameters tend to be application-specific, but oscillators with power consumption of less than 0.6 W and a mass of less than 0.4 kg are available.

1x10 14

1x10 13

1x10 12

1x10 11

1x10 10

0. 1 1 10Tau (s)

Sig

ma

100 1000

APL ultrastable quartz oscillator

Small military rubidium

High-performance cesium

High-performance rubidium

Quartz Oscillator CapabilityPerformance parameter ValuePrimary output frequency  5 MHzAging rate/24 h  7 × 10–13

Phase noise  Frequency offset (Hz)  1  –137 dBc  10  –149 dBc  100  –155 dBc  1,000  –158 dBc  10,000  –160 dBcFrequency as a function of   Temperature/°C     4 × 10–13

  Load  <1 × 10–12

  Input voltage  <1 × 10–12

CustomersInstitute of Space and Astronautical Science (ISAS), JapanJet Propulsion LaboratoryNASANaval Research LaboratoryU.S. Air ForceU.S. Navy

Potential ApplicationsSpace  Clocks  Frequency references  Radio science  Navigation  Event timers  Doppler beacons  Local oscillators for     communications     receivers

Space MissionsCassini  Mars Global ObserverCOBE   Mars ObserverCONTOUR   MSXDodge  New HorizonsDPCS  NOVAEUVE  Planet-B (Japan)Geosat  SAS    GEOS-C  SeasatGPSPAC   Topex/PoseidonGRACE  Transit 

Ground  Clocks  Frequency references  GPS timing systems  Calibration references  Test and measurement        equipment

Allan variance of precision frequency standards.

Duane DealDirector

National Security Space Programs 240-228-1633

[email protected]

07-00963-UQO.indd   2 3/13/07   2:11:56 PM