Pioneer 4
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| Pioneer 4 | |
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| Organization | NASA |
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| Mission type | Lunar flyby |
| Satellite of | Sun |
| Launch date | March 3, 1959 17:11:00 UTC |
| Launch vehicle | Juno II |
| NSSDC ID | 1959-013A |
| Mass | 6.1 kg |
| Orbital elements | |
| Eccentricity | 0.07109 |
| Inclination | 29.9° |
| Orbital period | 398.0 days |
| Apoapsis | 1.13 AU |
| Periapsis | 0.98 AU |
Pioneer 4 was a spin-stabilized 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. No lunar radiation was detected. The spacecraft was still in solar orbit as of 1969.
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[edit] 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.
[edit] Launching vehicle
Pioneer 4 was launched with a Juno II launching vehicle, which also launched Pioneer 3. Juno II closely resembled the Juno I (Jupiter-C based) vehicle that launched Explorer 1. Its first stage was a to 64 feet elongated Jupiter IRBM missile that was used in the army. On top of the Jupiter propulsion section was a guidance and control compartment that supported a rotating tub containing the rocket stages 2, 3 and 4. Pioneer 4 was mounted on top of stage 4.[1]
[edit] Mission
After a successful launch Pioneer 4 achieved its primary objective (an Earth-Moon trajectory), returned radiation data and provided a valuable tracking exercise. The probe passed within 60,000 km of the Moon's surface (7.2° E, 5.7° S) on 4 March 1959 at 22:25 UT (5:25 p.m. EST) at a speed of 7,230 km/h. The distance was not close enough to trigger the photoelectric sensor. The probe continued transmitting radiation data for 82 hours, to a distance of 658,000 km,[2] and reached perihelion on 18 March 1959 at 01:00 UT. The cylindrical fourth stage casing (173 cm long, 15 cm diameter, 4.65 kg) went into orbit with the probe.
[edit] References
- ^ Jet Propulsion Laboratory (under contract for NASA) (1959). "The Moon Probe Pioneer IV" (PDF). . NASA-JPL Retrieved on 2008-02-02.
- ^ Hess, Wilmot (1968). The Radiation Belt and Magnetosphere.
[edit] External links
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| Previous mission: Pioneer 3 | Next mission: Pioneer W |
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| Pioneer 0 · Pioneer 1 · Pioneer 2 · Pioneer 3 · Pioneer 4 · Pioneer P-1 (W) · Pioneer P-3 (X) · Pioneer P-30 (Y) · Pioneer P-31 (Z) | ||
| Pioneer 5 (P-2) · Pioneer 6, 7, 8 and 9 · Pioneer 10 · Pioneer 11 · Pioneer H · Pioneer Venus project | ||
