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Ranger 3



         


Ranger 3
Organization:NASA
Major Contractors: Jet Propulsion Laboratory
Mission Type: Lunar Science
Satellite of: Sun
Launch: January 26, 1962 at 20:30:00 UTC
Launch Vehicle: Atlas-Agena B
Decay: Flew past moon at 36,800 km distance on January 28, 1962,
now in heliocentric orbit.
Mission Duration: 2 days
Mass: 329.8 kg
NSSDC ID: 1962-001A
Webpage:
Orbital elements
Semimajor Axis: N/A
Eccentricity: N/A
Inclination: N/A
Orbital Period: N/A
Apogee: N/A
Perigee: N/A
Orbits: heliocentric orbit
Instruments
Television  : transmit closeup pictures of the lunar surface
Seismometer : determine the presence or absence of lunar seismicity


Ranger 3 was a spacecraft of the Ranger program that was launched to study the moon on January 26, 1962. The space probe was designed to transmit pictures of the lunar surface to Earth stations 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. Due to a series of malfunctions the spacecraft missed the Moon by 22,000 miles (35,000 km).

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Spacecraft design

Ranger 3 was the first of the so-called Block II Ranger designs. The basic vehicle was 3.1 m high and consisted of a lunar capsule covered with a balsa wood impact-limiter, 650 mm in diameter, a mono-propellant mid-course motor, a 5080 pound (22.6 kN) thrust retrorocket, and a gold- and chrome-plated hexagonal base 1.5 m in diameter. A large high-gain dish antenna was attached to the base. Two wing-like solar panels (5.2 m across) were attached to the base and deployed early in the flight. Power was generated by 8680 solar cells contained in the solar panels which charged a 11.5 kg 1 kWh capacity AgZn launching and backup battery. Spacecraft control was provided by a solid-state computer and sequencer and an earth-controlled command system. Attitude control was provided by Sun and Earth sensors, gyroscopes, and pitch and roll jets. The telemetry system aboard the spacecraft consisted of two 960 MHz transmitters, one at 3 W power output and the other at 50 mW power output, the high-gain antenna, and an omni-directional antenna. White paint, gold and chrome plating, and a silvered plastic sheet encasing the retrorocket furnished thermal control.

The experimental apparatus included: (1) a vidicon television camera, which employed a scan mechanism that yielded one complete frame in 10 s; (2) a gamma-ray spectrometer mounted on a 1.8 m boom; (3) a radar altimeter; and (4) a seismometer to be rough-landed on the lunar surface. The seismometer was encased in the lunar capsule along with an amplifier, a 50 mW transmitter, voltage control, a turnstile antenna, and 6 Ranger 2 Ranger program Next Mission:
Ranger 4

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