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IMP
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 | IMP-8 / Explorer 50 Credit - NASA
| Other Designations: Interplanetary Monitoring Platform. Class: Earth. Type: Magnetosphere. Destination: High Earth Orbit. Nation: USA. Agency: NASA. Manufacturer: NASA Goddard. The IMP series were managed by the Goddard Space Flight Center with the primary objectives of investigation of interplanetary plasma and the interplanetary magnetic field. The orbiting of IMP satellites in a variety of interplanetary and earth orbits allowed study of spatial and temporal relationships of geophysical and interplanetary phenomena simultaneously by several other National Aeronautics and Space Administration satellites. The IMP network provided a crucial 'early warning network' of solar flare activity for Apollo manned missions that ventured beyond the Van Allen Radiation Belts. Typical orbit: 56731 x 230661 km, 40.9 deg inclinaton. Associated Launch Vehicle: Delta 1000, Delta C, Delta E, Delta M. IMP Chronology
- 1965 May 4 - Three-station Apollo Solar Particle Alert Network ordered - Program: Apollo.
NASA Associate Administrator for Manned Space Flight George E. Mueller concurred with a plan of MSC Director Robert R. Gilruth to implement a three-station developmental Solar Particle Alert Network. Mueller said he understood that Gilruth would "review the necessity for the Guaymas station, and that you will examine having all data reduction related to this network carried out under contract," and adding that he felt the program would be enhanced if arrangement could be made to involve one or more academic institutions in the analysis of data.
- 1967 July 19 - Explorer 35 - Program: Explorer. Launch Site: Cape Canaveral. Launch Vehicle: Delta E. Mass: 104 kg (229 lb). Perigee: 484 km (300 mi). Apogee: 675 km (419 mi). Inclination: 32.40 deg. Period: 96.26 min.
Earth magnetic tail measurements. Lunar Orbit (Selenocentric). The Westinghouse Aerospace Division, under contract to National Aeronautics and Space Administration's Goddard Space Flight Center, engaged in the system design, integration, assembly and launch support for Anchored Interplanetary Monitoring Platform Satellite, officially designated Explorer 35 by the National Aeronautics and Space Administration. It was launched on July 19, 1967, with the primary objectives of investigation of interplanetary plasma and the interplanetary magnetic field out to and at the lunar distance, in either a captured lunar orbit or a geocentric orbit of the earth. In the geocentric orbit, the apogee was near or beyond the lunar distance. In a lunar orbit, additional objectives included obtaining data on dust distribution, lunar gravitational field, ionosphere, magnetic field, and radiation environment around the moon. AIMP-E also studied spatial and temporal relationships of geophysical and interplanetary phenomena simultaneously being studied by several other National Aeronautics and Space Administration satellites. The investigation in the vicinity of the moon provided for measurements of the characteristics of the interplanetary dust distribution, solar and galactic cosmic rays, as well as a study of the magnetohydrodynamic wake of the earth in the interplanetary medium at the lunar distances.
- 1972 September 23 - Explorer 47 - Program: Explorer. Launch Site: Cape Canaveral. Launch Vehicle: Delta 1000. Mass: 376 kg (828 lb). Perigee: 201,100 km (124,900 mi). Apogee: 235,600 km (146,300 mi). Inclination: 17.20 deg. Period: 17,670.00 min.
Investigated cislunar radiation, Earth's magnetosphere, interplantary magnetic field. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).
Bibliography and Further Reading
- Aerospace Yearbook, 1966, .
- McDowell, Jonathan, Jonathan's Space Home Page, Harvard University, 1997-present. Jonathan McDowell's complete on-line listing of all objects orbited and over 20,000 rocket launches Accessed at: http://www.planet4589.org/jsr.html.
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