Please make a donation to support Gunter's Space Page.
Thank you very much for visiting Gunter's Space Page. I hope that this site is useful and informative for you.
If you appreciate the information provided on this site, please consider supporting my work by making a simple and secure donation via PayPal. Please help to run the website and keep everything free of charge. Thank you very much.

IMP D, E (LAIMP 1, 2 / Explorer 33, 35)

Explorer-33 (IMP D) [NASA]

IMP D and E (Interplanetary Monitoring Platform), AIMP (Anchored Interplanetary Monitoring Platform) were spacecrafts instrumented for studies of interplanetary plasma, energetic charged particles, magnetic fields, and solar X-rays at lunar distances.

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 21 September 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 24 June 1973.

Nation: USA
Type / Application: Research, Magnetosphere
Operator: NASA
Propulsion: Star-13
Power: 4 deployable solar arrays, batteries
Mass: 93 kg (#D), 104 kg (#E)
Orbit: 265680 km × 480763 km, 24.4 (Lunar orbit planned) (#D); Lunar orbit (#E)
Satellite COSPAR Date LS Launch Vehicle Remarks
Explorer 33 (IMP D, AIMP 1) 1966-058A 01.07.1966 CC LC-17A Delta-E1
Explorer 35 (IMP E, AIMP 2) 1967-070A 19.07.1967 CC LC-17B Delta-E1


Cite this page: