Deep Space Atomic Clock

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Deep Space Atomic Clock (DSAC)
Deep Space Atomic Clock-DSAC.jpg
The miniaturized Deep Space Atomic Clock was designed for precise and real-time radio navigation in deep space
Operator Jet Propulsion Laboratory (JPL)
Manufacturer JPL
Instrument Type Atomic clock
Function Navigation aid in deep space, gravity and occultation science
Mission duration Planned: 1 year[1]
Website www.nasa.gov/mission_pages/tdm/clock/index.html
Properties
Mass 17.5 kg (39 lb)
Dimensions 29 × 26 × 23 cm[2]
(11 × 10 × 9 in)
Number launched 1
Power consumption 44 W
Host Spacecraft
Spacecraft Orbital Test Bed (OTB)
Launch date 25 June 2019[3]
Rocket Falcon Heavy
Launch Site LC-39A, Kennedy Space Center
Orbit Low Earth orbit

The Deep Space Atomic Clock (DSAC) is a miniaturized, ultra-precise mercury-ion atomic clock for precise radio navigation in deep space. It is orders of magnitude more stable than existing navigation clocks, and has been refined to limit drift of no more than 1 nanosecond in 10 days.[4] It is expected that a DSAC would incur no more than 1 microsecond of error in 10 years of operations.[5] It is expected to improve the precision of deep space navigation, and enable more efficient use of tracking networks. The project is managed by NASA's Jet Propulsion Laboratory and it was deployed as part of the U.S. Air Force's Space Test Program 2 (STP-2) mission aboard a SpaceX Falcon Heavy rocket on 25 June 2019.[3]

The Deep Space Atomic Clock was activated on 23 August 2019, according to NASA.[6]

Overview

Current ground-based atomic clocks are fundamental to deep space navigation, however, they are too large to be flown in space. This results in tracking data being collected and processed here on Earth (a two-way link) for most deep space navigation applications.[5] The Deep Space Atomic Clock (DSAC) is a miniaturized and stable mercury ion atomic clock that is as stable as a ground clock.[5] The technology could enable autonomous radio navigation for spacecraft's time-critical events such as orbit insertion or landing, promising new savings on mission operations costs.[4] It is expected to improve the precision of deep space navigation, enable more efficient use of tracking networks, and yield a significant reduction in ground support operations.[4][7]

Its applications in deep space include:[5]

  • Simultaneously track two spacecraft on a downlink with the Deep Space Network (DSN).
  • Improve tracking data precision by an order of magnitude using the DSN's Ka-band downlink tracking capability.
  • Mitigate Ka-band's weather sensitivity (as compared to two-way X band) by being able to switch from a weather-impacted receiving antenna to one in a different location with no tracking outages.
  • Track longer by using a ground antenna's entire spacecraft viewing period. At Jupiter, this yields a 10–15% increase in tracking; at Saturn, it grows to 15–25%, with the percentage increasing the farther a spacecraft travels.
  • Make new discoveries as a Ka-band—capable radio science instrument with a 10 times improvement in data precision for both gravity and occultation science and deliver more data because of one-way tracking's operational flexibility.
  • Explore deep space as a key element of a real-time autonomous navigation system that tracks one-way radio signals on the uplink and, coupled with optical navigation, provides for robust absolute and relative navigation.
  • Fundamental to human explorers requiring real-time navigation data.

Principle and development

Over 20 years, engineers at NASA's Jet Propulsion Laboratory have been steadily improving and miniaturizing the mercury-ion trap atomic clock.[8] The DSAC technology uses the property of mercury ions' hyperfine transition frequency at 40.50 GHz to effectively "steer" the frequency output of a quartz oscillator to a near-constant value. DSAC does this by confining the mercury ions with electric fields in a trap and protecting them by applying magnetic fields and shielding.[5][2]

Its development includes a test flight in low-Earth orbit,[9][10] while using GPS signals to demonstrate precision orbit determination and confirm its performance in radio navigation.

Deployment

The flight unit is being hosted —along with other four payloads— on a spacecraft called Orbital Test Bed (OTB) satellite, provided by General Atomics Electromagnetic Systems, using the Swift satellite bus.[11][12][13] It was deployed as a secondary spacecraft during the U.S. Air Force's Space Test Program 2 (STP-2) mission aboard a SpaceX Falcon Heavy rocket,[14] on 25 June 2019.[15]

References

  1. ↑ Deep Space Atomic Clock (DSAC). NASA's Space Technology Mission Directorate. Accessed on 10 December 2018.
  2. ↑ 2.0 2.1 Lua error in package.lua at line 80: module 'strict' not found.
  3. ↑ 3.0 3.1 Lua error in package.lua at line 80: module 'strict' not found.
  4. ↑ 4.0 4.1 4.2 Lua error in package.lua at line 80: module 'strict' not found.
  5. ↑ 5.0 5.1 5.2 5.3 5.4 Lua error in package.lua at line 80: module 'strict' not found.
  6. ↑ Lua error in package.lua at line 80: module 'strict' not found.
  7. ↑ Lua error in package.lua at line 80: module 'strict' not found.
  8. ↑ Lua error in package.lua at line 80: module 'strict' not found.
  9. ↑ Lua error in package.lua at line 80: module 'strict' not found.
  10. ↑ Lua error in package.lua at line 80: module 'strict' not found.
  11. ↑ Deep Space Atomic Clock (DSAC) Overview. NASA. Accessed on 10 December 2018.
  12. ↑ General Atomics Completes Ready-For-Launch Testing of Orbital Test Bed Satellite. General Atomics Electromagnetic Systems, press release on 3 April 2018.
  13. ↑ OTB: The Mission. Surrey Satellite Technology. Accessed on 10 December 2018.
  14. ↑ Lua error in package.lua at line 80: module 'strict' not found.
  15. ↑ Lua error in package.lua at line 80: module 'strict' not found.

External links

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