Description

This was a flight test of the Ranger spacecraft system designed for future lunar and interplanetary missions. Ranger 2 was designed to test various systems for future exploration and to conduct scientific observations of cosmic rays, magnetic fields, radiation, dust particles, and a possible hydrogen gas "tail" trailing the Earth.

Spacecraft and Subsytems

Spacecraft and Subsystems

Ranger 2 was of the Ranger Block 1 design and was almost identical to Ranger 1. The spacecraft consisted of a hexagonal base 1.5 m across upon which was mounted a cone-shaped 4 m high tower of aluminum struts and braces. Two solar panel wings measuring 5.2 m from tip to tip extended from the base. A high-gain directional dish antenna was attached to the bottom of the base.

Spacecraft experiments and other equipment were mounted on the base and tower. Instruments aboard the spacecraft included a Lyman-alpha telescope, a rubidium-vapor magnetometer, electrostatic analyzers, medium-energy-range particle detectors, two triple coincidence telescopes, a cosmic-ray integrating ionization chamber, cosmic dust detectors, and scintillation counters.

The communications system included the high gain antenna and an omni-directional medium gain antenna and two transmitters at approximately 960-mhz, one with 0.25 W power output and the other with 3 W power output. Power was to be furnished by 8680 solar cells on the two panels, a 53.5 kg silver-zinc battery, and smaller batteries on some of the experiments. Attitude control was provided by a solid-state timing controller, Sun and Earth sensors, gyroscopes, and pitch and roll jets. The temperature was controlled passively by gold plating, white paint, and polished aluminum surfaces.

The communications system included the high gain antenna and an omni-directional medium gain antenna and two transmitters, one at 960.1-mhz with 0.25 W power output and the other at 960.05-mhz with 3 W power output. Power was to be furnished by 8680 solar cells on the two panels, a 57 kg silver-zinc battery, and smaller batteries on some of the experiments. Attitude control was provided by a solid-state timing controller, Sun and Earth sensors, and pitch and roll jets. The temperature was controlled passively by gold plating, white paint, and polished aluminum surfaces.

Instruments

Lyman-Alpha Telescope

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Rubidium Vapor Magnetometer

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Electrostatic Analyzer

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Triple Coincident Telescope

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Charged Particle (Chicago)

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Cosmic Ray Ion Chamber

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Cosmic Dust Detectors

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Scintillation Counters

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Launch-Orbit Information

Launch Information

Launch Date: 1961-08-23 at 10:02:00 UTC
Launch Vehicle: Atlas-Agena B
Launch Site: Cape Canaveral, United States
Decay Date: 1961-08-30
Mass: 306.2 kg

Orbital Parameters

Type:ORbiter
Central Body: Earth
Epoch start: 1961-11-18 00:00:00 UTC
Epoch stop: 1961-11-20 00:00:00 UTC

Periapsis: 0 Apoapsis: Period: Inclination: 0° Eccentricity: 0

Mission Profile

The spacecraft was launched into a low earth parking orbit, but an inoperative roll gyro prevented Agena restart. The spacecraft could not be put into its planned deep-space trajectory, resulting in Ranger 2 being stranded in low earth orbit upon separation from the Agena stage. The orbit decayed and the spacecraft reentered Earth's atmosphere on 20 November 1961.

Total research, development, launch, and support costs for the Ranger series of spacecraft (Rangers 1 through 9) was approximately $170 million.

Summary