Ranger 1

Ranger 1

Ranger 1 Satellite in preparation for use at the Parade of Progress Show at the Public Hall, Cleveland, Ohio, August 1964
Mission type Technology
Operator NASA
Harvard designation 1961 Phi 1
SATCAT № 173
Mission duration 7 days
Spacecraft properties
Manufacturer Jet Propulsion Laboratory
Launch mass 306.2 kilograms (675 lb)
Start of mission
Launch date August 23, 1961, 06:02:00 UTC
Rocket Atlas LV-3 Agena-B
Launch site Cape Canaveral LC-12
End of mission
Decay date 30 August 1961
Orbital parameters
Reference system Geocentric
Regime Low Earth
(High Earth planned)
Semi-major axis 6,690.3 kilometres (4,157.2 mi)
Eccentricity 0.019939
Perigee 179 kilometres (111 mi)
Apogee 446 kilometres (277 mi)
Inclination 32.9 degrees
Period 91.1 minutes
Instruments
Lyman-Alpha Telescope
Magnetometer

Ranger 1 was a prototype spacecraft launched as part of the Ranger program of unmanned space missions. Its primary mission was to test the performance of those functions and parts necessary for carrying out subsequent lunar and planetary missions; a secondary objective was to study the nature of particles and fields in the space environment. Due to a launch failure, the spacecraft could only reach low Earth orbit, rather than the high Earth orbit that had been planned, and was only able to complete part of its mission.[1]

Spacecraft design

The spacecraft was of the Ranger Block 1 design and consisted of a hexagonal base 1.5-meter (4 ft 11 in) across upon which was mounted a cone-shaped 4 m high tower of aluminum struts and braces. Two solar panel wings measuring 5.2 metres (17 ft) 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 solar X-ray scintillation counters.[1]

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 watts power output and the other at 960.05 MHz with 3 watts power output. Power was to be furnished by 8680 solar cells on the two panels, a 57-kilogram (126 lb) 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.[1]

Mission

The Ranger 1 spacecraft was designed to go into an Earth parking orbit and then move into a 60,000-by-1,100,000-kilometre (37,000 by 684,000 mi) Earth orbit. The purpose was to test systems and strategies for future lunar missions.[1]

Launch delays

Launch

Ranger 1 was launched on August 23, 1961 atop an Atlas-Agena rocket. The first stage operated successfully, and the Agena B made its first burn to inject the satellite into a parking orbit; however the Agena's engine subsequently failed to restart to raise the satellite into the planned higher orbit, and Ranger 1 instead separated into low Earth orbit and began tumbling. The satellite re-entered Earth's atmosphere on August 30, 1961. While the spacecraft was still able to accomplish some flight testing objectives, little scientific data was returned.[1]

Footnotes

See also

References

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