HPDE.io

CRRES

ResourceID
spase://SMWG/Observatory/CRRES

Description

The Combined Release and Radiation Effects Satellite (CRRES) was launched into a geosynchronous
transfer orbit (GTO) for a nominal three-year mission to investigate fields, plasmas, and energetic particles
inside the Earth's magnetosphere. As part of the CRRES program the SPACERAD (Space Radiation Effects) project,
managed by Air Force Geophysics Laboratory, investigated the radiation environment of the inner and outer
radiation belts and measured radiation effects on state-of-the-art microelectronics devices. Other
magnetospheric, ionospheric, and cosmic ray experiments were included onboard CRRES and supported by NASA or
the Office of Naval Research. The chemical release project was managed by NASA/MSFC and utilized the release of
chemicals from onboard cannisters at low altitudes near dawn and dusk perigee times and at high altitudes near
local midnight. The chemical releases were monitored with optical and radar instrumentation by ground-based
observers to measure the bulk properties and movement of the expanding clouds of photo-ionized plasma along
field lines after the releases occurred. In order to study the magnetosphere at different local times during
the mission, the satellite orbit was designed to precess with respect to the earth-sun line such that the local
time at apogee decreased by 2.5 minutes/day from 08:00 (LT) just after launch and returned to this position in
nineteen-month cycles. The CRRES spacecraft had the shape of an octagonal prism with solar arrays on the top
side. The prism is 1 m high and 3 m between opposite faces. Four of the eight compartments were for the chemical
canisters and the other four housed SPACERAD and other experiments. The spacecraft body was spun at 2.2 rpm about
a spin axis in the ecliptic plane and kept pointed about 12 degrees ahead of the Sun's apparent motion in
celestial coordinates. Pre-launch and in-flight operations were supported by the Space Test and Transportation
Program Office of the U.S. Air Force Space Division. Contact with the CRRES spacecraft was lost on October 12,
1991 and was presumed to be due to onboard battery failure.

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Details

Version:2.2.0

Observatory

ResourceID
spase://SMWG/Observatory/CRRES
ResourceHeader
ResourceName
CRRES
AlternateName
1990-065A
AlternateName
Combined Release and Radiation Effects Satellite
ReleaseDate
2019-05-05 12:34:56Z
Description

The Combined Release and Radiation Effects Satellite (CRRES) was launched into a geosynchronous
transfer orbit (GTO) for a nominal three-year mission to investigate fields, plasmas, and energetic particles
inside the Earth's magnetosphere. As part of the CRRES program the SPACERAD (Space Radiation Effects) project,
managed by Air Force Geophysics Laboratory, investigated the radiation environment of the inner and outer
radiation belts and measured radiation effects on state-of-the-art microelectronics devices. Other
magnetospheric, ionospheric, and cosmic ray experiments were included onboard CRRES and supported by NASA or
the Office of Naval Research. The chemical release project was managed by NASA/MSFC and utilized the release of
chemicals from onboard cannisters at low altitudes near dawn and dusk perigee times and at high altitudes near
local midnight. The chemical releases were monitored with optical and radar instrumentation by ground-based
observers to measure the bulk properties and movement of the expanding clouds of photo-ionized plasma along
field lines after the releases occurred. In order to study the magnetosphere at different local times during
the mission, the satellite orbit was designed to precess with respect to the earth-sun line such that the local
time at apogee decreased by 2.5 minutes/day from 08:00 (LT) just after launch and returned to this position in
nineteen-month cycles. The CRRES spacecraft had the shape of an octagonal prism with solar arrays on the top
side. The prism is 1 m high and 3 m between opposite faces. Four of the eight compartments were for the chemical
canisters and the other four housed SPACERAD and other experiments. The spacecraft body was spun at 2.2 rpm about
a spin axis in the ecliptic plane and kept pointed about 12 degrees ahead of the Sun's apparent motion in
celestial coordinates. Pre-launch and in-flight operations were supported by the Space Test and Transportation
Program Office of the U.S. Air Force Space Division. Contact with the CRRES spacecraft was lost on October 12,
1991 and was presumed to be due to onboard battery failure.

Contacts
RolePersonStartDateStopDateNote
1.ProjectScientistspase://SMWG/Person/Susan.Gussenhoven-Shea
2.ProjectScientistspase://SMWG/Person/David.L.Reasoner
InformationURL
Name
NSSDC's Master Catalog
URL
Description

Information about the CRRES mission

InformationURL
Name
Journal of Spacecraft and Rockets Article
URL
Description

Detailed information on the CRRES mission.

Location
ObservatoryRegion
Earth.Magnetosphere.Main