Japanese Lunar Exploration Program km on opposite sides of the lunar body. The penetrators were to have been braked by a small rocket at an altitude of 25 km, then free fall to the surface. They were designed to withstand a collision speed of 330 meters per second to deeply penetrate the lunar regolith. Once the penetrators are deployed, the LUNAR-A spacecraft was mission-planned to maneuver to an orbital altitude of 200 km above the lunar surface. The craft was to have carried a monochromatic imaging camera with a resolution of 30 m. It was to be Japan's first large scale lunar probe. (Hiten
Explorer 15 between the spin axis and the sun direction to about 3° intervals. During launch the spacecraft failed to despin. The spin rate ranged from 72.9 to 73.2 rpm during the life of the spacecraft. The spin axis pointed at right ascension 80.97° and declination 20.9°. Explorer 15 Explorer 15, also called EPE-C, was an American satellite launched as part of Explorers program. Explorer 15 as launched on October 27, on Cape Canaveral Air Force Station, Florida, United States, with Delta rocket. Explorer 15 was a spin-stabilized, solar-cell powered spacecraft instrumented to study the artificial radiation belt produced by the Starfish