Explorer-33 (IMP D) [NASA] |
IMP (Interplanetary Monitoring Platform), AIMP (Anchored Interplanetary Monitoring Platform)
IMP D (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. 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. No data were obtained after September 21, 1971.
IMP E (Explorer 35) was a spin-stabilized spacecraft
instrumented for interplanetary studies, at lunar distances, of the interplanetary plasma,
magnetic field, energetic particles, and solar X rays. It was launched into an elliptical
lunar orbit. The spin axis direction was nearly perpendicular to the ecliptic plane, and
the spin rate was 25.6 rpm. Mission objectives were achieved. After successful operation
for 6 years, the spacecraft was turned off on June 24, 1973.
| Nation: | USA |
|---|---|
| Type / Application: | Research, Magnetosphere |
| Operator: | NASA |
| Contractors: | |
| Equipment: | |
| Configuration: | |
| Propulsion: | Star-13 |
| Lifetime: | |
| Mass: | 93 kg (#D), 104 kg (#E) |
| Orbit: | 265680 km x 480763 km, 24.4° (Lunar orbit planned) (#D); Lunar orbit (#E) |
| Satellite | Date | LS | Launcher | Remarks: | |
|---|---|---|---|---|---|
| Explorer 33 (IMP D, AIMP 1) | 01.07.1966 | CC LC-17A | Delta-E1 | ||
| Explorer 35 (IMP E, AIMP 2) | 19.07.1967 | CC LC-17B | Delta-E1 |
| Further IMP / ISEE missions: |
Source: NSSDC Master Catalog website
Last update: 27.09.2009
Contact: gunter.krebs@skyrocket.de
© Gunter Dirk Krebs