spase-metadata.org SPASE landing pages.

Explorer 33

ResourceID
spase://SMWG/Observatory/Explorer33

Description

NASA's Explorer 33 spacecraft, also known as
Anchored IMP A (AIMP A) and as IMP D, was launched into a geocentric
orbit in July, 1966. Explorer 33 was a spin-stabilized (spin axis
parallel to the ecliptic
plane, spin period varying between 2.2 and 3.6 s) spacecraft instrumented
for studies of interplanetary plasma, energetic charged particles
(electrons, protons, and alphas), magnetic fields, and solar X rays
at lunar distances. The spacecraft failed to achieve lunar orbit but
did achieve mission objectives. Lunar
perturbations caused significant variations in orbit parameters
The initial apogee occurred at about
1600 h local time. Over the first 3-yr period, perigee varied between
6 and 44 earth radii. Apogee varied between 70 and 135 earth radii,
and the inclination with respect to the equator of the earth varied
between 7 and 60 deg. Periods of principal data coverage (essentially
100%) are July 1, 1966 (launch), to January 14, 1970; February 21,
1970, to March 6, 1970; July 31, 1970, to September 14, 1970; January
15, 1971, to February 28, 1971; March 23, 1971, to May 31, 1971; and
August 23, 1971, to September 15, 1971. No data were obtained after
September 21, 1971.

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Details

Version:2.7.1

Observatory

ResourceID
spase://SMWG/Observatory/Explorer33
ResourceHeader
ResourceName
Explorer 33
AlternateName
IMP D
AlternateName
AIMP A
AlternateName
AIMP 1
AlternateName
02258
ReleaseDate
2026-07-20 16:22:40Z
RevisionHistory
RevisionEvent
ReleaseDate
2019-05-05 12:34:56Z
Note
Only known prior ReleaseDate of the metadata
RevisionEvent
ReleaseDate
2026-07-20 16:22:40Z
Note
Added HelioData InformationURL, Updated to SPASE Version 2.7.1. JWL
Description

NASA's Explorer 33 spacecraft, also known as
Anchored IMP A (AIMP A) and as IMP D, was launched into a geocentric
orbit in July, 1966. Explorer 33 was a spin-stabilized (spin axis
parallel to the ecliptic
plane, spin period varying between 2.2 and 3.6 s) spacecraft instrumented
for studies of interplanetary plasma, energetic charged particles
(electrons, protons, and alphas), magnetic fields, and solar X rays
at lunar distances. The spacecraft failed to achieve lunar orbit but
did achieve mission objectives. Lunar
perturbations caused significant variations in orbit parameters
The initial apogee occurred at about
1600 h local time. Over the first 3-yr period, perigee varied between
6 and 44 earth radii. Apogee varied between 70 and 135 earth radii,
and the inclination with respect to the equator of the earth varied
between 7 and 60 deg. Periods of principal data coverage (essentially
100%) are July 1, 1966 (launch), to January 14, 1970; February 21,
1970, to March 6, 1970; July 31, 1970, to September 14, 1970; January
15, 1971, to February 28, 1971; March 23, 1971, to May 31, 1971; and
August 23, 1971, to September 15, 1971. No data were obtained after
September 21, 1971.

Contacts
RolePersonStartDateStopDateNote
1.GeneralContactspase://SMWG/Person/Joseph.H.King
2.GeneralContactspase://SMWG/Person/Norman.F.Ness
InformationURL
InformationURL
Name
HelioData
URL
Description

The HelioData mission page provides an overview of the mission and more, such as all SPASE dataset records associated with it.

ObservatoryGroupID
Location
ObservatoryRegion
Heliosphere.NearEarth
ObservatoryRegion
Earth.Magnetosheath
ObservatoryRegion
Earth.Magnetosphere