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・ Pioneer mine
・ Pioneer Montessori Inter College
・ Pioneer Monument
・ Pioneer Monument (Houston)
・ Pioneer Monument (San Francisco)
・ Pioneer (video game)
・ Pioneer 0
・ Pioneer 1
・ Pioneer 1 (land speed racer)
・ Pioneer 10
・ Pioneer 11
・ Pioneer 12
・ Pioneer 2
・ Pioneer 2M
・ Pioneer 3
Pioneer 4
・ Pioneer 5
・ Pioneer 6, 7, 8, and 9
・ Pioneer Academy
・ Pioneer Academy, Puthimari
・ Pioneer Acres Museum
・ Pioneer Aerospace Corporation
・ Pioneer Amphitheatre
・ Pioneer and Endicott Buildings
・ Pioneer and Fayette Railroad
・ Pioneer and Military Memorial Park
・ Pioneer anomaly
・ Pioneer Arts Center of Easthampton
・ Pioneer Athletic Conference
・ Pioneer Award


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Pioneer 4 : ウィキペディア英語版
Pioneer 4

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Pioneer 4 was a spin-stabilized unmanned spacecraft launched as part of the Pioneer program on a lunar flyby trajectory and into a heliocentric orbit making it the first U.S. probe to escape from the Earth's gravity. It carried a payload similar to Pioneer 3: a lunar radiation environment experiment using a Geiger-Müller tube detector and a lunar photography experiment. It passed within 60,000 km of the Moon's surface. However, Pioneer 4 did not come close enough to trigger its photoelectric sensor. The spacecraft was still in solar orbit as of 1969. It was the only successful lunar probe launched by the US in seven attempts between 1958–60; only in 1963 would Ranger 6 surpass its success by accomplishing all of its mission objectives.
== Spacecraft design ==
Pioneer 4 was a cone-shaped probe 51 cm high and 23 cm in diameter at its base. The cone was composed of a thin fiberglass shell coated with a gold wash to make it electrically conducting and painted with white stripes to maintain the temperature between 10 and 50 degrees Celsius. At the tip of the cone was a small probe which combined with the cone itself to act as an antenna. At the base of the cone a ring of mercury batteries provided power. A photoelectric sensor protruded from the center of the ring. The sensor was designed with two photocells which would be triggered by the light of the Moon when the probe was within about 30,000 km of the Moon. At the center of the cone was a voltage supply tube and two Geiger-Müller tubes. A transmitter with a mass of 0.5 kg delivered a phase modulated signal of 0.1 W at a frequency of 960.05 MHz. The modulated carrier power was 0.08 W and the total effective radiated power 0.18 W. A despin mechanism consisted of two 7 gram weights which spooled out to the end of two 150 cm wires when triggered by a hydraulic timer 10 hours after launch. The weights were designed to slow the spacecraft spin from 400 rpm to 6 rpm, and then weights and wires were released.

抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
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