Julie Cooper is a certified archivist who identifies and processes collections for the JPL Archives, and helps researchers find information about the history of JPL.
This atomic clock was used at the Goldstone Time Standards Laboratory in 1970, to synchronize clocks at Deep Space Network stations around the world. This master clock was accurate to plus or minus two millionths of a second, when compared to clocks maintained by the National Bureau of Standards and the U.S. Naval Observatory. In the late 1960s, JPL had developed a moon bounce technique to transmit signals from one deep space antenna to another. Experiments included periodic measurement of timing signals that were reflected from the surface of the moon, to find out if the station clocks were within allowable limits for accuracy.
Professor James Van Allen of the University of Iowa designed the cosmic ray detector experiment on JPL’s Explorer satellite, launched in 1958. He was also the principal investigator for the radiation experiment that was part of the Pioneer III and IV payloads. In this photo, Dr. Van Allen is looking at the cone-shaped Pioneer probe, before it was gold plated and painted with stripes (to maintain a temperature of 10-50 degrees C during flight).
After the launch of Pioneer IV on March 3, 1959 the experiment successfully measured radiation found around the Earth. It was also designed to measure lunar radiation, but the flyby distance of 37,000 miles was not close enough for the optical trigger to work. The instrument used two Geiger-Mueller tubes to detect and measure radiation and a small battery-powered radio transmitter to send the data to Earth. The low-power signal was received by the 85-foot antenna at Goldstone, California -- part of what became known as the Deep Space Network in 1963. The probe also tested technology that would be needed for future lunar photographic missions. After passing by the moon, Pioneer IV went into a heliocentric orbit.
In 1943, JPL was under contract with the Army Air Corps to design, build and test an underwater solid rocket motor. Early tests were done in a large trough of water to see if a solid propellant would fire underwater ... and it did. Field tests were conducted in 1943 at the Morris Dam Test Facility in an artificial lake 25 miles from Pasadena, California. The facility was part of Caltech’s “other” rocket project, funded by the National Defense Research Committee of the Office of Scientific Research and Development – an agency set up to support and coordinate war-related research.
This photo shows a barge, which was anchored to trees on the shore of the lake, with an underwater structure that would hold the motor at a depth of one to six feet during testing. Two motion-picture cameras (one color, and one black and white) filmed the ten tests. The test motors were loaded with two different propellant formulas (GALCIT 53 and GALCIT 54).
JPL had a growing need for its own underwater test facility, so construction began on a hydrodynamic tank, or towing channel, in September 1943. It was located in the space currently occupied by the parking structure and part of Arroyo Road. An Army Air Forces contract for $121,000 – for development of a hydrobomb design – began in September 1944.
Most people know about the scenes, greetings, music and sounds from Earth found on the Voyager Golden Record. They may not know that there is also a handwritten message etched into the surface of the record. Timothy Ferris, who worked with Carl Sagan and the rest of the team that produced the record, wanted something done directly by a human hand to appear on the record. “To the makers of music – all worlds, all times” appears on the finished record, in between the photoengraved label and the record grooves.
The inscription can also be seen on some of the 14-inch recording masters that are found in the JPL Archives. There are several sets of the records, with a metal core and lacquer surface. From these masters, the copper records (“mothers”) were cut, then they were gold plated, etched, enclosed in aluminum containers and mounted on the sides of the Voyager 1 and 2 spacecraft.
In the early 1960s, Mesa Road at NASA's Jet Propulsion Laboratory had not yet been built. Access to buildings on the mesa, like the High Gain Antenna Tower in this photo, was through the residential neighborhood north of JPL.
The antenna tower was built at the end of 1961, and was used by the Telecommunications Division in testing prototypes and various configurations of Deep Space Network antenna equipment. The platform was designed to reduce ground reflections from the sides and bottom of the adjacent canyon.
This April 1962 photo of Deep Space Station 12 (DSS-12) in Goldstone, California, was featured in Space Programs Summary 37-15, Volume 3–The Deep Space Instrumentation Facility. The 85-foot (26-meter) Echo antenna can be seen through the window of the control room, and three unidentified men are at the controls. The Echo site was named for its support of Project Echo, an experiment that transmitted voice communications coast to coast by bouncing signals off the surface of a passive balloon-type satellite. The antenna was moved six miles in June 1962 to the Venus site (DSS-13) and in 1979 it was extended to 34 meters in diameter.
The bimonthly Space Programs Summary, or SPS, is an excellent source of information about JPL missions and related research from February 1959 to October 1970. In 1970, the SPS series was replaced by the Technical Reports (32-1 to 32-1606) and other report series.
In December 1954, only a few months after becoming the director of JPL, Dr. William Pickering (in the light-colored suit) hosted a visit by Frank H. Higgins, assistant secretary of the Army, and several members of his military entourage. At that time, JPL was under contract to Army Ordnance to develop guided missiles. In this photo, the group is gathered in the control room of the 20-inch wind tunnel. Frank Goddard (in the dark suit), chief of the Supersonic Aerodynamics Division, assisted with the tour and Bud Schurmeier, manager of the Wind Tunnel Section, observed from the back of the room while technicians conducted a demonstration.
In the early 1960s, a computer known as a coordinate converter was part of the instrumentation and equipment used to position the Deep Space Network, or DSN, antennas. This photograph from September 1960 shows a mechanical coordinate converter. The device converted azimuth-elevation position information to hour angle-declination and vice versa. It was able to coordinate two or more tracking antennas that used different coordinate systems for their pointing. It was likely used in early tracking studies of missiles and spacecraft, and as a visual backup for later antenna operations.
Patent US 3163935A lists JPL employee Richard M. Beckwith as the inventor of this instrument. In 1962, Beckwith was a designer with the Guidance and Control Design Group. The photo appears in the photo album for Communications Engineering and Operations, the JPL organization that managed the DSN antennas.
In October 1963, the Advanced Antenna System, also known as the 210-foot (64-meter) Mars antenna, was under construction at the Goldstone Deep Space Instrumentation Facility. The site was being cleared and a foundation dug, an access road was nearing completion, and a reservoir was built to provide water during construction. Assembly of the antenna required a 200-ton guy derrick, used to lift large pieces into place. In preparation for this stage of construction, scale models of the antenna and the guy derrick were built, showing how the derrick would be anchored to the desert floor by long cables.
In the early 1960s, a new large-aperture, low-noise Advanced Antenna System was in its planning and early development stages for the Deep Space Instrumentation Facility (later known as the Deep Space Network). Compared with the 85-ft (26-meter) antennas then in use, the new antenna was to give a 10-decibel performance increase, with an order of magnitude increase in the data rate from future spacecraft. Feasibility studies and testing were conducted by NASA's Jet Propulsion Laboratory in Pasadena, California, and subcontractors for various technologies and antenna components.
This January 1962 photo shows a 960-mc one-tenth scale Cassegrain antenna feed system study for the Advanced Antenna System. The objective was to establish the electrical performance capabilities and operational feasibility of this type of feed system for large antennas. The mount of the test system was covered with epoxy fiberglass and polystyrene foam to limit reflection of energy during testing.
A 210-foot (64-meter) antenna, using the new technology and designs, was built at the Goldstone site in California and became operational in 1966. The antenna, DSS 14, became known as the Mars antenna when it was used to track the Mariner 4 spacecraft. It was later upgraded to 70 meters in order to track Voyager 2 as it reached Neptune.