Explorer 35
| Explorer 35 / IMP-E | |
|---|---|
 | |
| Position | NASA |
| The main manufacturer | Langley Research Center |
| Duty | Selenography |
| It is targeted for go-around | Month |
| The launching date and time | July 19, 1967 14:19:02 UTC |
| Display machine | Delta DSV 3E1 |
| Term on duty | 2,167 days |
| COSPAR ID | 1967-070A |
| Mass | 104.3 kg |
| Orbital element | |
| Orbit semimajor axis | 7,886km |
| Orbit angle of inclination | 147.3 degrees |
| Distant visible point altitude | 7,886km |
| Perigee altitude | 764km |
| Orbit period | 710 minutes |
| The number of the day go-around | 4,395 |
| Deployment apparatus | |
| Main deployment apparatus | Magnetometer |
Explorer 35 (British: Explorer 35) is a lunar probe of the United States of America. On July 19, 1967, it was launched from Cape Canaveral Air Force Base. In moon elliptic orbit, I observed plasma, magnetic field, energy particle, sun X-rays. By posture control stable spin, the axis direction is approximately perpendicular to an ecliptic surface; the turn speed is 25.6 rpm. It is equipped with four pieces of solar panel.
This mission was a fresh start of Explorer 33 that failed in injection to lunar orbit. I succeed, and I manage it on June 24, 1973, and the mission stops.
References
- "Explorer 35". JAXA. March 5, 2010 reading.
- National Space Science Data Center Page on AIMP 2 (Explorer 35)
This article is taken from the Japanese Wikipedia Explorer 35
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