|
gptkbp:instanceOf
|
gptkb:military
data bus
|
|
gptkbp:alternativeName
|
1553 bus
MIL-STD-1553B
|
|
gptkbp:application
|
gptkb:aircraft
gptkb:Space_Shuttle
B-2 Spirit
|
|
gptkbp:bodyLength
|
20 bits per word
|
|
gptkbp:busController
|
centralized
|
|
gptkbp:compatibleWith
|
NATO forces
|
|
gptkbp:connectorType
|
circular military connectors
|
|
gptkbp:dataRate
|
1 Mbps
|
|
gptkbp:documentation
|
MIL-STD-1553B specification
|
|
gptkbp:errorDetection
|
parity
status word
|
|
gptkbp:firstPublished
|
1973
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
MIL-STD-1553 data bus
|
|
gptkbp:latestReleaseVersion
|
MIL-STD-1553C
|
|
gptkbp:length
|
16 data bits + 3 sync bits + 1 parity bit
|
|
gptkbp:maintenance
|
built-in test capability
|
|
gptkbp:maximumLength
|
shielded twisted pair
|
|
gptkbp:maxRemoteTerminals
|
31
|
|
gptkbp:messageType
|
gptkb:graphical_user_interface
gptkb:standard
data
|
|
gptkbp:operatingSystem
|
harsh environments
±7 to ±20 volts
|
|
gptkbp:physicalLayer
|
differential signaling
|
|
gptkbp:primaryUse
|
mission-critical communication
|
|
gptkbp:range
|
up to 100 meters
|
|
gptkbp:relatedStandard
|
gptkb:ARINC_429
STANAG 3838
|
|
gptkbp:replacedBy
|
MIL-STD-1553A
|
|
gptkbp:signalEncoding
|
Manchester II bi-phase
|
|
gptkbp:standardizedBy
|
gptkb:United_States_Department_of_Defense
|
|
gptkbp:supports
|
redundant bus architecture
|
|
gptkbp:supportsProtocol
|
command/response
|
|
gptkbp:topology
|
dual-redundant twisted pair
|
|
gptkbp:usedIn
|
gptkb:aircraft
gptkb:satellite
military avionics
|
|
gptkbp:bfsParent
|
gptkb:F-4E_AUP_Phantom_II
|
|
gptkbp:bfsLayer
|
8
|