Mission type | Navigation aid in deep space, gravity and occultation science |
---|---|
Operator | Jet Propulsion Laboratory / NASA |
COSPAR ID | 2019-036C |
SATCAT no. | 44341 |
Website | www |
Mission duration | Planned: 1 year [1] Final: 2 years and 26 days |
Spacecraft properties | |
Spacecraft | Orbital Test Bed (OTB) |
Manufacturer | General Atomics Electromagnetic Systems |
Payload mass | 17.5 kg |
Dimensions | 29 × 26 × 23 cm (11 × 10 × 9 in) |
Power | 44 watts |
Start of mission | |
Launch date | 25 June 2019, 06:30:00 UTC [2] |
Rocket | Falcon Heavy |
Launch site | KSC, LC-39A |
Contractor | SpaceX |
Entered service | 23 August 2019 |
End of mission | |
Disposal | Deactivated |
Deactivated | 18 September 2021 |
Orbital parameters | |
Reference system | Geocentric orbit |
Regime | Low Earth orbit |
Epoch | 25 June 2019 |
The Deep Space Atomic Clock (DSAC) was a miniaturized, ultra-precise mercury-ion atomic clock for precise radio navigation in deep space. DSAC was designed to be orders of magnitude more stable than existing navigation clocks, with a drift of no more than 1 nanosecond in 10 days. [3] It is expected that a DSAC would incur no more than 1 microsecond of error in 10 years of operations. [4] Data from DSAC is expected to improve the precision of deep space navigation, and enable more efficient use of tracking networks. The project was 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. [2]
The Deep Space Atomic Clock was activated on 23 August 2019. [5] Following a mission extension in June 2020, [6] DSAC was deactivated on 18 September 2021 after two years in operation. [7]
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. [4] The Deep Space Atomic Clock (DSAC) is a miniaturized and stable mercury ion atomic clock that is as stable as a ground clock. [4] 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. [3] 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. [3] [8]
Its applications in deep space include: [4]
Over 20 years, engineers at NASA's Jet Propulsion Laboratory have been steadily improving and miniaturizing the mercury-ion trap atomic clock. [3] 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. [4] [9]
Its development includes a test flight in low Earth orbit, [10] while using GPS signals to demonstrate precision orbit determination and confirm its performance in radio navigation.
The Deep Space Atomic Clock-2, an improved version of the DSAC, will fly on the VERITAS mission to Venus in 2028. [11]
The flight unit is being hosted — along with other four payloads — on the Orbital Test Bed satellite, provided by General Atomics Electromagnetic Systems, using the Swift satellite bus. [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 on 25 June 2019. [2]
An ion thruster, ion drive, or ion engine is a form of electric propulsion used for spacecraft propulsion. An ion thruster creates a cloud of positive ions from a neutral gas by ionizing it to extract some electrons from its atoms. The ions are then accelerated using electricity to create thrust. Ion thrusters are categorized as either electrostatic or electromagnetic.
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Time History of Events and Macroscale Interactions during Substorms (THEMIS) mission began in February 2007 as a constellation of five NASA satellites to study energy releases from Earth's magnetosphere known as substorms, magnetic phenomena that intensify auroras near Earth's poles. The name of the mission is an acronym alluding to the Titan Themis.
OSTM/Jason-2, or Ocean Surface Topography Mission/Jason-2 satellite, was an international Earth observation satellite altimeter joint mission for sea surface height measurements between NASA and CNES. It was the third satellite in a series started in 1992 by the NASA/CNES TOPEX/Poseidon mission and continued by the NASA/CNES Jason-1 mission launched in 2001.
C/NOFS, or Communications/Navigation Outage Forecasting System was a USAF satellite developed by the Air Force Research Laboratory (AFRL) Space Vehicles Directorate to investigate and forecast scintillations in the Earth's ionosphere. It was launched by an Orbital Sciences Corporation Pegasus-XL launch vehicle at 17:02:48 UTC on 16 April 2008 and decayed on 28 November 2015.
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The forerunner of the Deep Space Network was established in January 1958, when JPL, then under contract to the U.S. Army, deployed portable radio tracking stations in Nigeria, Singapore, and California to receive telemetry and plot the orbit of the Army-launched Explorer 1, the first successful U.S. satellite.
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