About: Spacecraft bus (James Webb Space Telescope)

Facets (new session)
Description
Metadata
Settings
- Rule:
- Inverse Functional Properties:
- "Same As":

About: Spacecraft bus (James Webb Space Telescope) Goto Sponge NotDistinct Permalink

An Entity of Type : owl:Thing, within Data Space : dbpedia.demo.openlinksw.com associated with source document(s)
QRcode icon

http://dbpedia.demo.openlinksw.com/describe/?url=http%3A%2F%2Fdbpedia.org%2Fresource%2FSpacecraft_bus_%28James_Webb_Space_Telescope%29&invfp=IFP_OFF&sas=SAME_AS_OFF

The spacecraft bus is the primary support element of the James Webb Space Telescope, launched on 25 December 2021. It hosts a multitude of computing, communication, propulsion, and structural components. The other three elements of the JWST are the Optical Telescope Element (OTE), the Integrated Science Instrument Module (ISIM) and the sunshield. Region 3 of ISIM is also inside the spacecraft bus. Region 3 includes the ISIM Command and Data Handling subsystem and the Mid-Infrared Instrument (MIRI) cryocooler.

Attributes	Values
rdfs:label	Spacecraft bus (James Webb Space Telescope) (en)
rdfs:comment	The spacecraft bus is the primary support element of the James Webb Space Telescope, launched on 25 December 2021. It hosts a multitude of computing, communication, propulsion, and structural components. The other three elements of the JWST are the Optical Telescope Element (OTE), the Integrated Science Instrument Module (ISIM) and the sunshield. Region 3 of ISIM is also inside the spacecraft bus. Region 3 includes the ISIM Command and Data Handling subsystem and the Mid-Infrared Instrument (MIRI) cryocooler. (en)
foaf:depiction
dcterms:subject	James Webb Space Telescope
Wikipage page ID	52566668 (xsd:integer)
Wikipage revision ID	1104986743 (xsd:integer)
Link from a Wikipage to another Wikipage	MIRI (Mid-Infrared Instrument) MIL-STD-1553 On-board data handling Algorithm Hubble Space Telescope Hydrazine Lithium-ion battery Integrated Science Instrument Module Orbital station-keeping Optical Telescope Element Minute of arc Cryocooler Spacecraft thermal control James Webb Space Telescope °C °F Fuel tank Hemispherical resonator gyroscope Deep Space Network Star tracker Sunlight Buck converter Actuator Helium Northrop Grumman Graphite Reaction wheel Halo orbit Attitude control James Webb Space Telescope James Webb Space Telescope timeline Telemetry Ariane 5 Kelvin Sunshield (JWST) Honeycomb structure Dinitrogen tetroxide Spacecraft design Thrusters (spacecraft) Redondo Beach, California Satellite bus Space Telescope Science Institute Gyroscope Reaction wheels SpaceWire Solar panels on spacecraft Ka-band S-band
Link from a Wikipage to an external page	http://media.globenewswire.com/noc/mediagallery.html%3Fpkgid=36796 https://www.cosmos.esa.int/documents/739790/758041/ClampinM.pdf/ab03f396-5d69-4495-bfe4-c226d5642f42
sameAs	Spacecraft bus (James Webb Space Telescope) Spacecraft bus (James Webb Space Telescope)
dbp:wikiPageUsesTemplate	dbt:Blockquote dbt:Chem2 dbt:Citation_needed dbt:Convert dbt:Frac dbt:Nbsp dbt:Reflist dbt:Rp dbt:Short_description dbt:N2O4 dbt:Jwstnav
thumbnail	wiki-commons:Special:FilePath/Mockup_of_JWST_bus_009.jpg?width=300
has abstract	The spacecraft bus is the primary support element of the James Webb Space Telescope, launched on 25 December 2021. It hosts a multitude of computing, communication, propulsion, and structural components. The other three elements of the JWST are the Optical Telescope Element (OTE), the Integrated Science Instrument Module (ISIM) and the sunshield. Region 3 of ISIM is also inside the spacecraft bus. Region 3 includes the ISIM Command and Data Handling subsystem and the Mid-Infrared Instrument (MIRI) cryocooler. The spacecraft bus must structurally support the 6.5 ton space telescope, while weighing only 350 kg (770 lb). It is made primarily of graphite composite material. It was assembled in the U.S. state of California by 2015, and then it had to be integrated with the rest of the space telescope leading up to its planned 2018 launch. The bus can provide pointing precision of one arcsecond (1⁄3600°) and isolates vibration down to two milliarcseconds. The fine pointing is done by the JWST fine guidance mirror, obviating the need to physically move the whole mirror or bus. The spacecraft bus is on the Sun-facing "warm" side and operates at a temperature of about 300 kelvins (80 °F, 27 °C). Everything on the Sun-facing side must be able to handle the thermal conditions of JWST's halo orbit, which has one side of continuous sunlight and the other shaded by the spacecraft sunshield. Another important aspect of the spacecraft bus is the central computing, memory storage, and communications equipment. The processor and software direct data to and from the instruments, to the solid-state memory core, and to the radio system which can send data back to Earth and receive commands. The computer also controls the pointing and movement of the spacecraft, taking in sensor data from the gyroscopes and star tracker, and sending the necessary commands to the reaction wheels or thrusters. (en)
prov:wasDerivedFrom	wikipedia-en:Spacecraft_bus_(James_Webb_Space_Telescope)?oldid=1104986743&ns=0
page length (characters) of wiki page	26627 (xsd:nonNegativeInteger)
foaf:isPrimaryTopicOf	wikipedia-en:Spacecraft_bus_(James_Webb_Space_Telescope)
is Link from a Wikipage to another Wikipage of	MIRI (Mid-Infrared Instrument) Integrated Science Instrument Module Optical Telescope Element Spacecraft Bus (JWST) Spacecraft Bus (James Webb Space Telescope) Spacecraft Bus - JWST Spacecraft bus (JWST) Fine Guidance Sensor and Near Infrared Imager and Slitless Spectrograph Spacecraft bus - JWST
is Wikipage redirect of	Spacecraft Bus (JWST) Spacecraft Bus (James Webb Space Telescope) Spacecraft Bus - JWST Spacecraft bus (JWST) Spacecraft bus - JWST
is foaf:primaryTopic of	wikipedia-en:Spacecraft_bus_(James_Webb_Space_Telescope)

Faceted Search & Find service v1.17_git139 as of Feb 29 2024

Alternative Linked Data Documents: ODE Content Formats:

RDF

ODATA

Microdata

About

OpenLink Virtuoso version 08.03.3330 as of Mar 19 2024, on Linux (x86_64-generic-linux-glibc212), Single-Server Edition (378 GB total memory, 60 GB memory in use)
Data on this page belongs to its respective rights holders.
Virtuoso Faceted Browser Copyright © 2009-2024 OpenLink Software