Movatterモバイル変換


[0]ホーム

URL:


Jump to content
WikipediaThe Free Encyclopedia
Search

LISA Pathfinder

From Wikipedia, the free encyclopedia
2015 European Space Agency spacecraft
LISA Pathfinder
LISA Pathfinder spacecraft
Model of theLISA Pathfinder spacecraft
Mission typeHigh-precision metrology, Technology demonstrator for gravitational-wave observation
OperatorESA[1]
COSPAR ID2015-070AEdit this at Wikidata
SATCATno.41043Edit this on Wikidata
Mission duration576 days
Spacecraft properties
ManufacturerAirbus Defence and Space
Launch mass1,910 kg (4,210 lb)[1]
BOL mass480 kg (1,060 lb)[2]
Dry mass810 kg (1,790 lb)
Payload mass125 kg (276 lb)
Dimensions2.9 m × 2.1 m (9.5 ft × 6.9 ft)
Start of mission
Launch date3 December 2015, 04:04:00 UTC[3][4][5]
RocketVega (VV06)
Launch siteKourouELV
ContractorArianespace
End of mission
DisposalDecommissioned
Deactivated30 June 2017
Orbital parameters
Reference systemSun–Earth L1
RegimeLissajous orbit
Periapsis altitude500,000 km (310,000 mi)
Apoapsis altitude800,000 km (500,000 mi)
Inclination60 degrees
EpochPlanned
Transponders
BandX band
Bandwidth7 kbit/s
Instruments
~36.7 cm Laserinterferometer
LISA Pathfinder insignia
ESA astrophysics insignia forLISA Pathfinder
← Gaia

LISA Pathfinder (LPF) was a space mission by theEuropean Space Agency (ESA). It was launched on 3 December 2015 on boardVega flight VV06, and operated until July 2017.[3][4][5] The mission tested key technologies needed for theLaser Interferometer Space Antenna (LISA), an ESAgravitational wave observatory planned to be launched in 2035.[6] Formerly, the mission was known as Small Missions for Advanced Research in Technology-2 (SMART-2) of theSmall Missions for Advanced Research in Technology ESA scientific programme. The LISA Pathfinder scientific phase started on 1 March 2016 and lasted almost sixteen months.[7][8] In June 2016, ESA announced that LISA Pathfinder demonstrated that the LISA mission is feasible,[9] paving the way for the official adoption of the LISA mission.[10]

The mission cost was €490 million.[11] It involved research institutes and space companies from many European countries, as well as the AmericanNational Aeronautics and Space Administration (NASA).[12][13]

Mission

[edit]

LISA Pathfinder was a proof-of-concept mission, to prove that the two masses (known as test masses) can fly through space, untouched but shielded by the spacecraft, and maintain their relative positions to the precision needed to realize a full gravitational wave observatory. The primary objectives were to minimize the external forces acting on the test masses, guaranteeing small deviations fromgeodesic motion, and to measure their relative displacement with high precision. Much of the experimentation ingravitational physics requires measuring the relative acceleration between free-falling, geodesic reference test particles.[14]

LISA Pathfinder hosted the first sub-picometerlaserinterferometer ever flown in space,[15] capable of tracking the relative displacement of the two test masses, situated about 38 cm apart in a single spacecraft. For the gravitational wave observatoryLISA,[16] each of three separate spacecraft will host two test masses, 2.5 million kilometers apart.[17] The science of LISA Pathfinder consisted of measuring and creating an experimentally-anchored physical model for all the spurious effects – including stray forces and optical measurement limits – that limit the ability to create, and measure, the perfect constellation of free-falling test particles that would be ideal for theLISA follow-up mission.[18]

LISA will have its test mass pairsfree falling along the spacecraft-to-spacecraft axes, with micro-Newtonthrusters controlling the spacecraft motion to follow the test masses. In LISA Pathfinder, however, the complete free fall was not possible, as the two test masses were enclosed in the same spacecraft. Hence, the spacecraft could follow only one of the two masses in its free fall, and was forced to applyfeedback forces to the second test mass. This way, the spacecraft acted as an active shield to external noisy forces, especially the solar radiation pressure, whose magnitude would prevent the mission to reach its requirements. The main LISA Pathfinder science measurement was therefore the out-of-loop differentialacceleration between the two test masses.

One of the two gold-platinum test masses, used as gravitational references and laser end-mirrors on LISA Pathfinder.

Spacecraft design

[edit]

LISA Pathfinder was assembled byAirbus Defence and Space in Stevenage (UK), under contract to the European Space Agency. It carried a European "LISA Technology Package" comprising inertial sensors, interferometer and associated instrumentation as well as two drag-free control systems: a European one using cold gas micro-thrusters (similar to those used onGaia), and a US-built "Disturbance Reduction System" using the European sensors and anelectric propulsion system that uses ionised droplets of a colloid accelerated in anelectric field.[19] Thecolloid thruster (or "electrospray thruster") system was built byBusek and delivered toJPL for integration with the spacecraft.[20]

LISA Pathfinder exploded view

Instrumentation

[edit]

The LISA Technology Package (LTP) was integrated by Airbus Defence and Space Germany, but the instruments and components were supplied by contributing institutions across Europe. The noise rejection technical requirements on the interferometer were very stringent, which means that the physical response of the interferometer to changing environmental conditions, such as temperature, must be minimised.

Spacecraft operations

[edit]

Mission control for LISA Pathfinder was atESOC inDarmstadt, Germany with science and technology operations controlled fromESAC inMadrid, Spain.[21]

Lissajous orbit

[edit]

The spacecraft was first launched byVega flight VV06 into an ellipticalLEO parking orbit. From there it executed a short burn each timeperigee was passed, slowly raising theapogee closer to the intendedhalo orbit around the Earth–SunL1 point.[1][22][23]

Animation of LISA Pathfinder's trajectory
Polar view
Equatorial view
Viewed from the Sun
   Earth ·   LISA Pathfinder

Chronology and results

[edit]
The final results (red line) far exceeded from the initial requirements.

The spacecraft reached its operational location in orbit around theLagrange point L1 on 22 January 2016, where it underwent payload commissioning.[24] The testing started on 1 March 2016.[25] In April 2016 ESA announced that LISA Pathfinder demonstrated that the LISA mission is feasible.[26]

On 7 June 2016, ESA presented the first results of two months' worth of science operation showing that the technology developed for a space-based gravitational wave observatory was exceeding expectations. The two cubes at the heart of the spacecraft are falling freely through space under the influence of gravity alone, unperturbed by other external forces, to a factor of 5 better than requirements for LISA Pathfinder.[27][28][29] In February 2017, BBC News reported that the gravity probe had exceeded its performance goals.[30]

LISA Pathfinder was deactivated on 30 June 2017.[31]

See also

[edit]
  • Einstein Telescope, a European gravitational wave detector
  • GEO600, a gravitational wave detector located in Hannover, Germany
  • LIGO, a gravitational wave observatory in USA
  • Taiji 1, a Chinese technology demonstrator for gravitational wave observation launched in 2019
  • Virgo interferometer, an interferometer located close to Pisa, Italy

References

[edit]
  1. ^abc"LISA Pathfinder: Operations".ESA. 8 January 2010. Retrieved5 February 2011.
  2. ^"LPF (LISA Pathfinder) Mission".ESA eoPortal. Archived fromthe original on 2015-10-17. Retrieved2014-03-28.
  3. ^ab"Launch Schedule". SpaceFlight Now. Archived fromthe original on 2016-12-24. Retrieved2015-10-16.
  4. ^ab"Call for Media: LISA Pathfinder launch". ESA. 23 November 2015.
  5. ^ab"LISA Pathfinder enroute to gravitational wave demonstration".European Space Agency. Retrieved3 December 2015.
  6. ^"LISA factsheet".www.esa.int. Retrieved2025-07-13.
  7. ^"News: Top News - LISA Gravitational Wave Observatory". Archived fromthe original on 2016-04-19.
  8. ^LISA Pathfinder Collaboration; Armano, M.; Audley, H.; Baird, J.; Binetruy, P.; Born, M.; Bortoluzzi, D.; Castelli, E.; Cavalleri, A.; Cesarini, A.; Chiavegato, V.; Cruise, A. M.; Dal Bosco, D.; Danzmann, K.; De Deus Silva, M. (2024-08-21)."In-depth analysis of LISA Pathfinder performance results: Time evolution, noise projection, physical models, and implications for LISA".Physical Review D.110 (4) 042004.arXiv:2405.05207.Bibcode:2024PhRvD.110d2004A.doi:10.1103/PhysRevD.110.042004.
  9. ^"Green light for space-based gravitational wave detector".www.science.org. Retrieved2025-07-13.
  10. ^"Capturing the ripples of spacetime: LISA gets go-ahead".www.esa.int. Retrieved2025-07-13.
  11. ^Mike Wall (2016-06-07)."Near-Perfect Free Fall in Space Sets Stage for Gravitational Wave Hunt".Space. Retrieved2025-07-13.
  12. ^"LISA Pathfinder international partners".eLISAscience.org. Archived fromthe original on 26 September 2015. Retrieved7 September 2015.
  13. ^"ESA Science & Technology - Industrial contributions to LISA Pathfinder".sci.esa.int. Retrieved2025-07-13.
  14. ^science objective of LISA PathfinderArchived 2014-10-21 at theWayback Machine.
  15. ^Armano, M.; Audley, H.; Baird, J.; Binetruy, P.; Born, M.; Bortoluzzi, D.; Brandt, N.; Castelli, E.; Cavalleri, A.; Cesarini, A.; Cruise, A. M.; Danzmann, K.; de Deus Silva, M.; Diepholz, I.; Dixon, G. (2021-04-02)."Sensor Noise in LISA Pathfinder: In-Flight Performance of the Optical Test Mass Readout".Physical Review Letters.126 (13) 131103.Bibcode:2021PhRvL.126m1103A.doi:10.1103/PhysRevLett.126.131103.hdl:10261/261499.PMID 33861094.
  16. ^"LISA Gravitational Wave Observatory - We will observe gravitational waves in space - New Astronomy - LISA Pathfinder".
  17. ^Official design proposal athttps://www.elisascience.org/files/publications/LISA_L3_20170120.pdfArchived 2017-10-17 at theWayback Machine
  18. ^"LISA Pathfinder Science".eLISAscience.org. Archived fromthe original on 21 October 2014. Retrieved9 July 2014.
  19. ^Ziemer, J.K.; and Merkowitz, S.M.: "Microthrust Propulsion of the LISA Mission," AIAA–2004–3439, 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Fort Lauderdale FL, July 11–14, 2004.
  20. ^Rovey, J."Propulsion and Energy: Electric Propulsion (Year in Review, 2009)"(PDF). Aerospace America, December 2009, p. 44. Archived fromthe original(PDF) on 2015-12-08. Retrieved2012-10-26.
  21. ^"LISA Pathfinder: Fact sheet".ESA. Retrieved20 April 2009.
  22. ^"LISA Pathfinder: Mission home".ESA. Retrieved5 February 2011.
  23. ^"ESA's new vision to study the invisible universe".www.esa.int. Retrieved26 June 2014.
  24. ^"First locks released from LISA Pathfinder's cubes".ESA. ESA Press Release. February 3, 2016. Retrieved2016-02-12.
  25. ^Amos, Jonathan (1 March 2016)."Gravitational waves: Tests begin for future space observatory".BBC News. Retrieved2016-03-01.
  26. ^Gravitational Observatory Advisory Team, ed. (28 March 2016).The ESA–L3 Gravitational Wave Mission - Final Report(PDF). ESA–L3 Final Report. p. 4.
  27. ^M. Armano; et al. (2016)."Sub-Femto-g Free Fall for Space-Based Gravitational Wave Observatories: LISA Pathfinder Results".Physical Review Letters.116 (23) 231101.Bibcode:2016PhRvL.116w1101A.doi:10.1103/PhysRevLett.116.231101.hdl:2117/102419.PMID 27341221.
  28. ^"LISA Pathfinder exceeds expectations". ESA. 7 June 2016. Retrieved7 June 2016.
  29. ^"LISA Pathfinder exceeds expectations".Benjamin Knispel. elisascience.org. 7 June 2016. Archived fromthe original on 3 August 2016. Retrieved7 June 2016.
  30. ^"Gravity probe exceeds performance goals".Jonathan Amos, BBC Science Correspondent, Boston. 18 February 2017. Retrieved20 February 2017.
  31. ^"LISA Pathfinder Will Concludee Trailblazing Mission".ESA Science and Technology. ESA. 20 June 2017. Retrieved17 August 2017.

External links

[edit]
Wikimedia Commons has media related toLISA Pathfinder.
Space Centres
Launch vehicles
Facilities
Communications
Programmes
Predecessors
Related topics
Science
Astronomy
& cosmology
Earth
observation
Planetary
science
Solar
physics
Human
spaceflight
Telecommunications
and navigation
Technology
demonstration
and education
Launch
and reentry
Proposed
Cancelled
Failed
Future missions initalics
Operating
Radio and
Microwave
Infrared
Optical
Ultraviolet
X-ray and
Gamma-ray
Other
(particle or
unclassified)
Planned
Proposed
Retired
Hibernating
(Mission completed)
Lost/Failed
Cancelled
Related
Detectors
Resonant mass
antennas
Active
Past
Proposed
Past proposals
Ground-based
interferometers
Active
Past
Planned
Proposed
Past proposals
Space-based
interferometers
Planned
Proposed
Pulsar timing arrays
Data analysis
Observations
Events
Methods
Theory
Effects/properties
Types/sources
21st-centuryspace probes
Active space probes
(deep space missions)
Sun
Moon
Mars
Other planets
Minor planets
Interstellar space
Completed after 2000
(by termination date)
2000s
2010s
2020s
January
February
March
April
May
June
July
August
September
October
November
December
Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ).
Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).
2015 in space
Space probe launchesSpace probes launched in 2015
Space probes
Space observatories
  • DSCOVR (weather satellite; Feb 2015)
  • Astrosat (space telescope; Sep 2015)


Impact events
SelectedNEOs
ExoplanetsExoplanets discovered in 2015
Discoveries
CometsComets in 2015
Space exploration
Retrieved from "https://en.wikipedia.org/w/index.php?title=LISA_Pathfinder&oldid=1322263839"
Categories:
Hidden categories:

[8]ページ先頭

©2009-2025 Movatter.jp