EQUULEUS CubeSat

E309956

EQUULEUS CubeSat is a small Japanese-led spacecraft designed to demonstrate low-energy trajectory techniques and study Earth's plasmasphere from cislunar space.

All labels observed (1)

Label Occurrences
EQUULEUS CubeSat canonical 1

How this entity was disambiguated

Statements (48)

Predicate Object
instanceOf CubeSat ⓘ
deep space CubeSat ⓘ
spacecraft ⓘ
abbreviation EQUULEUS ⓘ
affiliation JAXA Institute of Space and Astronautical Science ⓘ
University of Tokyo Intelligent Space Systems Laboratory ⓘ
attitudeControl three-axis stabilized ⓘ
communicationBand S-band ⓘ
X-band ⓘ
countryOfOrigin Japan ⓘ
deploymentLocation trans-lunar injection orbit of Artemis I ⓘ
developedBy JAXA ⓘ
University of Tokyo ⓘ
fullName EQUilibriUm Lunar-Earth point 6U Spacecraft ⓘ
instrumentPurpose CLOTH supports optical navigation and attitude determination ⓘ
DELPHINUS detects micrometeoroid and debris impacts ⓘ
PHOENIX observes Earth’s plasmasphere in extreme ultraviolet ⓘ
launchConfiguration secondary payload ⓘ
launchDate 2022-11-16 ⓘ
launchedWithMission Artemis I ⓘ
launchSite Kennedy Space Center LC-39B ⓘ
launchVehicle Space Launch System Block 1 ⓘ
linked to: Space Launch System
mass approximately 14 kilograms ⓘ
missionStatus operational ⓘ
missionType space science ⓘ
technology demonstration ⓘ
operator JAXA ⓘ
orbits Earth–Moon system ⓘ
payload CLOTH camera for optical navigation ⓘ
DELPHINUS dust detector ⓘ
PHOENIX extreme ultraviolet imager ⓘ
powerSource solar panels ⓘ
primaryObjective demonstrate low-energy trajectory techniques in cislunar space ⓘ
observe and study Earth’s plasmasphere from cislunar space ⓘ
program Artemis I secondary payloads ⓘ
propulsionType low-thrust propulsion ⓘ
water-resistojet propulsion ⓘ
scienceObjective characterize the structure of the Earth’s plasmasphere ⓘ
monitor variations in the plasmasphere over time ⓘ
spacecraftBus 6U CubeSat ⓘ
studies Earth’s plasmasphere dynamics ⓘ
space plasma environment ⓘ
targetRegion Earth–Moon Lagrange region ⓘ
cislunar space ⓘ
technologyDemonstrated low-energy cislunar transfers with CubeSats ⓘ
water-based propulsion in deep space ⓘ
usesTrajectoryTechnique ballistic lunar transfer ⓘ
low-energy trajectory ⓘ

How these facts were elicited

Referenced by (1)

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

Artemis I → carriedPayload → EQUULEUS CubeSat ⓘ