Mission type | Lunar impactor | ||||||||||
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Operator | NASA | ||||||||||
Harvard designation | 1962 Alpha 1 | ||||||||||
COSPAR ID | 1962-001A | ||||||||||
SATCAT no. | 221 | ||||||||||
Mission duration | Launch to last scientific data transmitted 1.405 days; launch day to official mission end day 5 days | ||||||||||
Spacecraft properties | |||||||||||
Manufacturer | Jet Propulsion Laboratory | ||||||||||
Launch mass | 330 kg [1] | ||||||||||
Power | 150 W | ||||||||||
Start of mission | |||||||||||
Launch date | January 26, 1962, 20:30:00[1] | UTC||||||||||
Rocket | Atlas LV-3B Agena-B | ||||||||||
Launch site | Cape Canaveral LC-12 | ||||||||||
End of mission | |||||||||||
Last contact | Last scientific data transmitted between 12:52 and 1:33 a.m. EST, January 28, 1962[2] | ||||||||||
Orbital parameters | |||||||||||
Reference system | Heliocentric | ||||||||||
Eccentricity | 0.083 | ||||||||||
Perihelion altitude | 0.9839 astronomical units (147,190,000 km) | ||||||||||
Aphelion altitude | 1.163 astronomical units (174,000,000 km) | ||||||||||
Inclination | 0.398° | ||||||||||
Period | 406.4 days | ||||||||||
Lunar flyby (failed impact) | |||||||||||
Closest approach | January 28, 1962 | ||||||||||
Distance | 36,874 kilometers (22,912 mi) | ||||||||||
| |||||||||||
Ranger 3 was a space exploration mission conducted by NASA to study the Moon. The Ranger 3 robotic spacecraft was launched January 26, 1962 as part of the Ranger program. Due to a series of malfunctions, the spacecraft missed the Moon by 22,000 miles (35,000 km) and entered a heliocentric orbit.[4][5]
The Ranger 3 space probe was designed to transmit pictures of the lunar surface during a period of 10 minutes of flight prior to impacting on the Moon, to rough-land a seismometer capsule on the Moon, to collect gamma-ray data in flight, to study radar reflectivity of the lunar surface, and to continue testing of the Ranger program for development of lunar and interplanetary spacecraft.