Injun 5 (Explorer 40) was a 71-kg magnetically oriented spacecraft and was launched by a Scout rocket, together with a
3.65-m inflatable balloon (Explorer 39) used for air density measurements. Injun 5 was designed to accomplish the following objectives:
(1) comprehensive study of the downward flux of charged particles, (2) study of very low frequency (VLF) radio emission in the ionosphere
associated with the downward flux, (3) study of geomagnetically trapped protons, alpha particles, and electrons, (4) observation of solar
cosmic rays, (5) observation of the continuing decay of the Starfish artificial radiation belt, and (6) study of the temperature and density
of electrons and positive ions of thermal and near thermal energy. The spacecraft systems performed normally except for the malfunction of
the solar cell power dump device (shortly after launch) which caused the solar cells to deliver a lower power level to the experiments and
reduced the time during which the onboard tape recorder could be run. The passive magnetic alignment became effective in mid-December 1968.
The spacecraft was turned off from May 31, 1970, to February 18, 1971, after this period it was turned on again. The spacecraft was put in
an operational off-mode in early June 1971, and became inoperable shortly thereafter.
Version:2.2.2
Injun 5 (Explorer 40) was a 71-kg magnetically oriented spacecraft and was launched by a Scout rocket, together with a
3.65-m inflatable balloon (Explorer 39) used for air density measurements. Injun 5 was designed to accomplish the following objectives:
(1) comprehensive study of the downward flux of charged particles, (2) study of very low frequency (VLF) radio emission in the ionosphere
associated with the downward flux, (3) study of geomagnetically trapped protons, alpha particles, and electrons, (4) observation of solar
cosmic rays, (5) observation of the continuing decay of the Starfish artificial radiation belt, and (6) study of the temperature and density
of electrons and positive ions of thermal and near thermal energy. The spacecraft systems performed normally except for the malfunction of
the solar cell power dump device (shortly after launch) which caused the solar cells to deliver a lower power level to the experiments and
reduced the time during which the onboard tape recorder could be run. The passive magnetic alignment became effective in mid-December 1968.
The spacecraft was turned off from May 31, 1970, to February 18, 1971, after this period it was turned on again. The spacecraft was put in
an operational off-mode in early June 1971, and became inoperable shortly thereafter.
Role | Person | StartDate | StopDate | Note | |
---|---|---|---|---|---|
1. | PrincipalInvestigator | spase://SMWG/Person/James.A.Van.Allen |
Information about the Injun 5 mission