STEREO

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Spacecraft subsystems

Dry mass Miniature inertial measurement unit Honeywell Ring laser gyroscopes Star tracker

20 related topics

Mission profile

Cape Canaveral Air Force Station Delta II Elliptical Geocentric orbits Apogee

14 related topics

Mission benefits

Solar wind Plasma Sunspots Helioseismology Madhulika Guhathakurta

10 related topics

Science instrumentation

Coronagraphs Corona Heliospheric imagers Energetic particles Janet Luhmann

9 related topics

Key facts & relationships

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Contractor: United Launch Alliance
COSPAR ID: STEREO-A: 2006-047A STEREO-B: 2006-047Bn
Dimensions: 1.14 × 2.03 × 6.47 m 3.75 × 6.67 × 21.24 ft
Dry mass: 547 kg (1,206 lb)
IMPACT: In-situ Measurements of Particles and CME Transients
Instruments: InstrumentsSECCHISun Earth Connection Coronal and Heliospheric InvestigationIMPACTIn-situ Measurements of Particles and CME TransientsPLASTICPlasma and Suprathermal Ion Composit…

Topics to explore

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Overview

Sun
Stereoscopic
Coronal mass ejections Coronal mass ejection

Mission profile

Cape Canaveral Air Force Station
Delta II
Elliptical Ellipse
Geocentric orbits Geocentric orbit
Apogee Apsis
Gravity assist
Heliocentric orbit
Quadrature Quadrature (astronomy)
Lagrangian points Lagrangian point
L5 Lagrange point
Lagrangian (trojan) asteroids Trojan (celestial body)
Solar Dynamics Observatory
Reaction wheels Reaction wheel
Deep Space Network NASA Deep Space Network

Mission benefits

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Map overview Semantic statistics

Nodes69

Edges68

Triples141

Avg. degree1.97

Density0.028986

Components1

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STEREO

Top relations

related to Science instrumentation · 32

STEREO → Antoinette Galvin, CME Transients, COR1, COR2, Each, Earth, EUVI, Heliospheric Investigation, HI1, HI2, IMPACT, In-situ Measurements, Janet Luhmann, Jean Louis Bougeret, Michael Kaiser, Particles, PLAsma, PLASTIC, Russell Howard, SCIP

related to Mission profile · 21

STEREO → Because, Cape Canaveral Air Force, Delta II, Earth, Earth's, Florida, Given, January, Launch Pad, Moon, Moon's, October, On December, Spacecraft, Station, STEREO-B Earth The, Sun, Sun/Earth, The, Their

related to Gallery · 20

STEREO → Astrotech, Delta II, Deputy Project Scientist Terry, Earth, February, Florida August, Kucera, March, Material, Moon, October, STEREO December, STEREO March, STEREO's, STEREO-A HI1 November, STEREO-B's, Sun, Sun February, Sun's South Pole, The Moon

related to External links · 14

STEREO → Applied Physics LaboratorySTEREO Science, Center, CME Archived May, Comet Encke, Goddard Space Flight CenterSTEREO, NASAInstrument, NASASTEREO/SECCHI Comets, Naval Research LaboratoryHeliospheric Imager, Rutherford Appleton LaboratoryCometsTail, Science, Sungrazer Project, The First, Wayback Machine, Years

related to Mission benefits · 12

STEREO → Because, Before STEREO, CMEs, Earth, Earth's, NASA, Since, Sun, Sun's, The, The STEREO, This

related to Spacecraft subsystems · 11

STEREO → Additional, Each STEREO, Honeywell, In, MIMU, SECCHI Guide Telescope, The, The STEREO, These, Upon, With

related to Loss of contact with STEREO-B · 6

STEREO → Deep Space Network, Later, NASA, On October, STEREO-B, The

Mission duration · 3

STEREO → Planned: 2 years, STEREO-A elapsed: 19 years, 9 months, 29 days, STEREO-B final: 9 years, 10 months, 30 days

Contractor · 1

STEREO → United Launch Alliance

COSPAR ID · 1

STEREO → STEREO-A: 2006-047A STEREO-B: 2006-047Bn

Important terminology Word statistics

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Important terminology

spacecraft solar sun earth stereo-b launched contact orbit mission power nasa mass earth's side two coronal stereo-a 21 secchi august

Entity relationships Subject–Predicate–Object triples

Subject	Predicate	Object	Confidence	Src
STEREO	Contractor	United Launch Alliance	1.00	infobox
STEREO	COSPAR ID	STEREO-A: 2006-047A STEREO-B: 2006-047Bn	1.00	infobox
STEREO	Dimensions	1.14 × 2.03 × 6.47 m 3.75 × 6.67 × 21.24 ft	1.00	infobox
STEREO	Dry mass	547 kg (1,206 lb)	1.00	infobox
STEREO	IMPACT	In-situ Measurements of Particles and CME Transients	1.00	infobox
STEREO	Instruments	InstrumentsSECCHISun Earth Connection Coronal and Heliospheric InvestigationIMPACTIn-situ Measurements of Particles and CME TransientsPLASTICPlasma and Suprathermal Ion Composit…	1.00	infobox
STEREO	Last contact	STEREO-B: September 23, 2016	1.00	infobox
STEREO	Launch date	October 26, 2006, 00:52 (2006-10-26UTC00:52) UTC	1.00	infobox
STEREO	Launch mass	STEREO-A: 620 kg STEREO-B: 620 kg	1.00	infobox
STEREO	Launch site	Cape Canaveral SLC-17B	1.00	infobox
STEREO	Manufacturer	Johns Hopkins University Applied Physics Laboratory	1.00	infobox
STEREO	Mission duration	Planned: 2 years	1.00	infobox
STEREO	Mission duration	STEREO-A elapsed: 19 years, 9 months, 29 days	1.00	infobox
STEREO	Mission duration	STEREO-B final: 9 years, 10 months, 30 days	1.00	infobox
STEREO	Mission type	Solar observation	1.00	infobox
STEREO	Operator	NASA	1.00	infobox
STEREO	Period	STEREO-A: 346 days STEREO-B: 388 days	1.00	infobox
STEREO	PLASTIC	Plasma and Suprathermal Ion Composition	1.00	infobox
STEREO	Power	475 W	1.00	infobox
STEREO	Reference system	Heliocentric	1.00	infobox
STEREO	Rocket	Delta II 7925-10L	1.00	infobox
STEREO	S/WAVES	STEREO/WAVES	1.00	infobox
STEREO	SATCAT no.	STEREO-A: 29510 STEREO-B: 29511	1.00	infobox
STEREO	SECCHI	Sun Earth Connection Coronal and Heliospheric Investigation	1.00	infobox
STEREO	Website	stereo.gsfc.nasa.gov stereo.jhuapl.edu	1.00	infobox

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