AMPTE-UKS

AMPTE-UKS
NamesAMPTE-United Kingdom Subsatellite
Mission typeMagnetosphere research
OperatorNASA / United Kingdom
COSPAR ID1984-088C Edit this at Wikidata
SATCAT no.15201
Mission duration5 months (achieved)
Spacecraft properties
SpacecraftAMPTE-UKS
Spacecraft typeActive Magnetospheric Particle Tracer Explorers (AMPTE)
BusAMPTE-United Kingdom Subsatellite
ManufacturerRutherford Appleton Laboratory
Launch mass77 kg (170 lb)
Start of mission
Launch date16 August 1984, 14:48 UTC[1]
RocketDelta 3924 (Delta 175)
Launch siteCape Canaveral, LC-17A
ContractorDouglas Aircraft Company
Entered service16 August 1984
End of mission
Last contact15 January 1985
Orbital parameters
Reference systemGeocentric orbit[2]
RegimeHighly elliptical orbit
Perigee altitude550 km (340 mi)
Apogee altitude112,800 km (70,100 mi)
Inclination28.50°
Period2630.00 minutes
Instruments
3-D Electron Analyzer (6 eV-25 keV, 8-Sector, 5-seconds Averaged)
3-D Ion Analyzer (10 eV-20 keV/Q, 12-Sector, 5-seconds Averaged)
Particle Modulation Analyzer (1 Hz-1 MHz Fast Fourier Transform)
Plasma Wave Spectrometer (100 Hz-3 MHz E, 100 Hz-60 kHz B)
Triaxial Magnetometer (Dual Range 0.03 nT Accuracy)
Cosmic Background Explorer (Explorer 66) →

AMPTE-UKS, also called AMPTE-United Kingdom Subsatellite, was a United Kingdom satellite designed and tasked to study the magnetosphere of Earth, being launched as part of the Explorer program. The AMPTE (Active Magnetospheric Particle Tracer Explorers) mission was designed to study the access of solar wind ions to the magnetosphere, the convective-diffusive transport and energization of magnetospheric particles, and the interactions of plasmas in space.[3]

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