A2100-derived GPS III bus

E786508

The A2100-derived GPS III bus is a modernized satellite platform based on Lockheed Martin’s A2100 series, specifically adapted to support the advanced navigation, timing, and anti-jamming requirements of the U.S. Air Force’s GPS III satellites.

All labels observed (8)

How this entity was disambiguated

Statements (48)

Predicate Object
instanceOf satellite bus ⓘ
adaptedFor medium Earth orbit navigation missions ⓘ
attitudeControl three-axis stabilized ⓘ
basedOn Lockheed Martin A2100 satellite bus ⓘ
countryOfOrigin United States ⓘ
designedForConstellation GPS III ⓘ
linked to: GPS

GPS III Follow-On (GPS IIIF) ⓘ
designedForLifetime 15 years or more ⓘ
designedToMeet enhanced anti-jam performance requirements ⓘ
improved integrity monitoring requirements ⓘ
modernized GPS accuracy requirements ⓘ
developer Lockheed Martin ⓘ
feature enhanced pointing accuracy ⓘ
improved thermal control ⓘ
increased payload power ⓘ
modular design ⓘ
radiation-hardened electronics ⓘ
secure command and telemetry links ⓘ
heritageFrom A2100 geostationary communications satellite bus ⓘ
improvesUpon Block IIF GPS satellite bus ⓘ
Block IIR GPS satellite bus ⓘ
manufacturer Lockheed Martin Space ⓘ
operator United States Space Force ⓘ
orbitType medium Earth orbit ⓘ
originalCustomer United States Air Force ⓘ
powerGenerationType solar arrays ⓘ
propulsionType chemical propulsion ⓘ
monopropellant thrusters ⓘ
supportsCapability anti-jamming ⓘ
nuclear detonation detection payloads ⓘ
search and rescue payloads ⓘ
supportsMissionType navigation ⓘ
positioning ⓘ
timing ⓘ
supportsPayload advanced GPS navigation payload ⓘ
supportsSignal L1C civil signal ⓘ
L2C civil signal ⓘ
L5 safety-of-life signal ⓘ
M-code military signal ⓘ
typicalOrbitAltitude about 20,200 kilometers ⓘ
usedFor GPS III satellite series ⓘ
usedInProgram Global Positioning System ⓘ
linked to: GPS
usedOnSpacecraft GPS III SV01 ⓘ
GPS III SV02 ⓘ
GPS III SV03 ⓘ
GPS III SV04 ⓘ
GPS III SV05 ⓘ
GPS III SV06 ⓘ

How these facts were elicited

Referenced by (9)

Full triples — surface form annotated when it differs from this entity's canonical label.

A2100 → hasVariant → A2100-derived GPS III bus ⓘ
B1061 → launchedMission → GPS III SV05 ⓘ
linked to: A2100-derived GPS III bus
A2100-derived GPS III bus → designedForConstellation → GPS III Follow-On (GPS IIIF) ⓘ
linked to: A2100-derived GPS III bus
A2100-derived GPS III bus → usedOnSpacecraft → GPS III SV01 ⓘ
linked to: A2100-derived GPS III bus
A2100-derived GPS III bus → usedOnSpacecraft → GPS III SV02 ⓘ
linked to: A2100-derived GPS III bus
A2100-derived GPS III bus → usedOnSpacecraft → GPS III SV03 ⓘ
linked to: A2100-derived GPS III bus
A2100-derived GPS III bus → usedOnSpacecraft → GPS III SV04 ⓘ
linked to: A2100-derived GPS III bus
A2100-derived GPS III bus → usedOnSpacecraft → GPS III SV05 ⓘ
linked to: A2100-derived GPS III bus
A2100-derived GPS III bus → usedOnSpacecraft → GPS III SV06 ⓘ
linked to: A2100-derived GPS III bus